JP2010255418A - Combination engine with various energy conservation cycle - Google Patents

Combination engine with various energy conservation cycle Download PDF

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JP2010255418A
JP2010255418A JP2009101707A JP2009101707A JP2010255418A JP 2010255418 A JP2010255418 A JP 2010255418A JP 2009101707 A JP2009101707 A JP 2009101707A JP 2009101707 A JP2009101707 A JP 2009101707A JP 2010255418 A JP2010255418 A JP 2010255418A
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turbine
liquid metal
compressed air
heat
right angle
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Hiroyasu Tanigawa
浩保 谷川
Kazunaga Tanigawa
和永 谷川
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/46Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines

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Abstract

<P>PROBLEM TO BE SOLVED: To drive out the existing power generation to prevent global heating by generating electricity by injection output of rotation output of 10,000 to 23,000 times a liquid metal solar engine. <P>SOLUTION: In the liquid metal solar engine, the moving blade groups of a plurality of turbines are formed to have the same diameter and approximately the same shape with respect to each turbine stage and are assembled by fitting bolts, the turbines are respectively driven by liquid metal gravity acceleration, partial overheated steam acceleration and partial combustion gas acceleration, liquid metal power having the same speed and the same volume as the atmospheric pressure is set to be 10,000 to 23,000 times stronger than rotation output of the existing steam turbine, most superheated steam and combustion gas are supplied to a combined engine injection section 78S, and fuel is injected and burnt, thereby making pressure of 10 to 100 times the existing jet airplane, heat quantity injection of 10 times thereof and injection thrust power of 100 to 1,000 times thereof reach space in a short time. Consequently, various large airships, various airplanes and various aircraft are driven, fuel consumption is reduced, CO2 emissions are reduced, use of space is achieved, finite resources such as fossil fuel are left to posterity, and also the global heating is prevented. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

本発明はスクラムジェットエンジンやロケットエンジン等の長所と合体し、特に蒸気タービンの排気温度20度Cに近付く最大膨張速度と合体高温燃焼ガスで加熱して、20度に近付く過熱蒸気を500度等に上昇膨張速度を更に増大し、最高の組み合わせにした合体機関噴射部78Sとして、過熱蒸気50製造の過程では太陽光加熱空気を圧縮1200度に近付け熱交換過熱蒸気を製造し、製造の過程で燃料噴射燃焼熱交換過熱蒸気50を製造する操作を複数回実施して、理論最良の推進剤過熱蒸気50無限製造と空燃比縮小に挑戦し、過熱蒸気50噴射の過程では燃焼器1Y燃料噴射燃焼1200度等として、外周過熱蒸気溜95cの過熱蒸気50を加熱最高温度にして噴射の過程で、過熱蒸気50の外周に設けた複数の燃焼ガス噴射ノズル6Y高温高速燃焼内に燃料噴射2段燃焼し、過熱蒸気50の外周を1200度に近付けて20度に近付く過熱蒸気を加熱して、過熱蒸気容積を増大して噴射推進出力と燃焼ガス49の吸引出力を増大し、燃焼ガス吸引出力の増大により燃焼ガス噴射ノズル6Yの3段燃焼を可能にして、環状の燃焼ガス噴射ノズル6Y高速燃焼内に複数の燃料噴射ノズル6Xより燃料噴射3段燃焼し、最も効率の良い空燃比燃焼や噴射推進出力を最も安価な太陽光+安価燃料燃焼にして、過熱蒸気製造複数燃焼を含めた合体機関噴射部78S3段燃焼とし、非常に安価な宇宙利用全盛を狙う合体機関噴射部78S等の技術に関する。   The present invention is combined with the advantages of a scramjet engine, a rocket engine, etc., and particularly heated at a maximum expansion speed approaching an exhaust temperature of steam turbine 20 ° C. and a combined high-temperature combustion gas, superheated steam approaching 20 ° In the process of manufacturing superheated steam 50, solar heating air is brought close to compression 1200 degrees in the process of manufacturing superheated steam 50, and heat exchange superheated steam is manufactured. The fuel injection combustion heat exchange superheated steam 50 is produced several times to challenge the theoretically best propellant superheated steam 50 infinite production and air-fuel ratio reduction. In the process of superheated steam 50 injection, combustor 1Y fuel injection combustion A plurality of combustion gas injection nozzles provided on the outer periphery of the superheated steam 50 in the process of injection with the superheated steam 50 in the outer peripheral superheated steam reservoir 95c at the highest heating temperature, such as 1200 degrees. 6Y fuel injection two-stage combustion in high-temperature high-speed combustion, the superheated steam 50 is heated to close to the outer periphery of the superheated steam 50 and approaches 20 degrees, the superheated steam volume is increased, the injection propulsion output and the combustion gas 49 The combustion gas injection nozzle 6Y can perform three-stage combustion by increasing the combustion gas suction output, and the three stages of fuel injection from the plurality of fuel injection nozzles 6X in the high-speed combustion of the annular combustion gas injection nozzle 6Y. Combustion, the most efficient air-fuel ratio combustion and injection propulsion output is the cheapest sunlight + cheap fuel combustion, combined engine injection part 78S three-stage combustion including multiple combustion of superheated steam production, very inexpensive space utilization The present invention relates to a technique such as a united engine injection unit 78S aiming for prime.

燃料費僅少の宇宙往還機等で燃料費0の宇宙利用全盛を狙うもので、大気中では太陽光で加熱した空気を、竪型全動翼液体金属太陽熱タービン駆動熱ポンプ1Gで吸入圧縮熱交換熱回収して、必要に応じて圧縮熱交換熱回収複数回の過程で燃料噴射燃焼熱交換過熱蒸気50を製造し、酸化剤の圧縮空気28a質量乃至燃焼ガス49質量と推進剤の過熱蒸気50を製造して、太陽系宇宙では圧縮空気の減圧循環使用と太陽光120度Cと長レンズ2dにより過熱蒸気製造効率を大幅に上昇し、宇宙上昇時は圧縮空気28a製造で過熱蒸気50製造の過程で複数回燃料噴射燃焼して、24〜400MPa過熱蒸気製造量を増大して合体機関噴射部78S燃焼器1Yに供給燃料噴射燃焼し、24〜400MPa燃焼ガス49を複数の燃焼ガス噴射ノズル6Yより噴射して、高圧高速噴射により前方の空気を強力に吸引衝撃波の発生を不要とした燃料噴射2段燃焼にし、更に過熱蒸気50の高圧高速噴射による強力な吸引力を利用した燃料噴射3段燃焼にして、理論空燃比に近付け最も安価な燃焼ガス推進剤と過熱蒸気推進剤を最も効率良く噴射し、蒸気タービンの大膨張速度とスクラムジェットの高速燃焼を合体した合体機関噴射部78Sとして、既存ジェット機の10〜100倍圧力10倍熱量噴射100〜1000倍噴射出力狙いの、竪型全動翼液体金属重力太陽熱タービン8G複数駆動合体機関噴射部78Sにし、実験最良エンジンに移行温度管理の竪型全動翼液体金属太陽熱タービン技術に関する。 Aiming for space-use prime with a low fuel cost, such as a space-return vehicle with a small fuel cost, air heated by sunlight in the atmosphere is suction-compressed and heat-exchanged with a 1G full-blade liquid metal solar turbine driven heat pump 1G Heat recovery is performed to produce the fuel-injection combustion heat exchange superheated steam 50 in the course of multiple times of compression heat exchange heat recovery as required, and the compressed air 28a mass of combustion agent to 49 masses of combustion gas and the superheated steam 50 of propellant. In the solar system space, the superheated steam production efficiency is significantly increased by the use of compressed air under reduced pressure circulation, sunlight 120 degrees C and the long lens 2d. When the space rises, the process of producing superheated steam 50 by producing compressed air 28a The fuel is injected and burned a plurality of times to increase the production amount of 24-400 MPa superheated steam, and the supplied fuel is injected and burned into the combined engine injection unit 78S combustor 1Y. The fuel is injected from the cylinder 6Y, and the high-speed high-speed injection is used to make the front air powerfully the fuel injection two-stage combustion that does not require the generation of the suction shock wave, and further, the fuel injection using the strong suction force by the high-pressure high-speed injection of the superheated steam 50 Combining engine injection unit 78S that combines the large expansion speed of the steam turbine and the high-speed combustion of the scramjet by performing the three-stage combustion, injecting the most inexpensive combustion gas propellant and superheated steam propellant close to the stoichiometric air-fuel ratio As a vertical all-blade liquid metal gravity solar turbine 8G multi-drive coalescence engine injection unit 78S, aiming at an injection output of 10 to 100 times pressure 10 times calorie injection 100 to 1000 times that of existing jets, and transition temperature management to the best engine of experiment This is related to the vertical all-blade liquid metal solar thermal turbine technology.

液体金属熱量駆動タービン+液体金属質量駆動タービン大気中は重力追加駆動とし、合金を含む液体金属を水銀・液体鉛・液体ビスマス・液体錫・液体カドミウム・液体インジウム・液体ガリウム・液体亜鉛・液体タリウム等として、タービン駆動の過程では液体金属噴射ポンプ6Lで400MPa等噴射し、最適温度液体金属を圧縮空気熱量+圧縮空気質量で加速して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にしたタービン翼8cに噴射し、夫々を液体金属の転がり接触回転出力の増大として、タービン間に横軸1hを設けて、横軸1h発電機1や横軸1h熱ポンプ1G多数で圧縮空気熱量+質量無限製造にタービン外箱77a外で挑戦し、複数の竪型全動翼液体金属太陽熱タービン8G回転方向交互で振動や騒音を相殺僅少にして、熱量駆動質量駆動タービンで熱ポンプ1G駆動、長レンズ2d熱吸収材2Bで構成の吸入空気路28A太陽熱加熱の空気28aを吸入し、圧縮800〜1200度にして圧縮熱回収器2Cにより別空気28aを500度前後に加熱して、熱ポンプで吸入圧縮熱回収を繰り返して圧縮空気28a製造と熱製造を無限継続膨大とし、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン出力の1〜2.3万倍液体金属出力として、合体機関噴射部78Sを駆動、実験最良に移行する液体金属太陽熱エンジン技術に関する。 Liquid metal calorie drive turbine + liquid metal mass drive turbine In the atmosphere, gravity is added to drive, and liquid metals including alloys are mercury, liquid lead, liquid bismuth, liquid tin, liquid cadmium, liquid indium, liquid gallium, liquid zinc, and liquid thallium. In the turbine driving process, 400MPa is injected by the liquid metal injection pump 6L, the optimum temperature liquid metal is accelerated by the amount of heat of compressed air + the amount of compressed air, and the turbine blade cross section 4X is 2 to 26 times that of the existing steam turbine. The turbine blades 8c are each injected to increase the rolling contact rotation output of the liquid metal, and the horizontal axis 1h is provided between the turbines. The amount of compressed air is increased by the horizontal axis 1h generator 1 and the horizontal axis 1h heat pump 1G + Challenges for infinite mass production outside the turbine outer casing 77a, and cancels vibration and noise by alternately rotating the multiple vertical rotor blades liquid metal solar thermal turbine 8G. Then, the heat pump 1G is driven by the heat driven mass driven turbine, the intake air passage 28A composed of the long lens 2d and the heat absorbing material 2B is sucked into the solar heating air 28a, compressed to 800 to 1200 degrees by the compression heat recovery device 2C. Heating the separate air 28a to around 500 degrees and repeating the suction compression heat recovery with a heat pump to make the compressed air 28a production and heat production endlessly enormous, The present invention relates to a liquid metal solar engine technology that drives the combined engine injection unit 78S as the liquid metal output 1 to 230,000 times the output of the existing steam turbine and makes the best transition to the experiment.

後追いエンジン発明阻止のため、高校や大学で既存エンジンを理論最良エンジンと巧妙に騙しており、小学校理科に戻って理論最良エンジンを考えると、馬力や仕事率の単位がkg重m/秒等重量×速度のため、重い物質を高速度にして回転出力発生が理論最良エンジンです。更に火力原子力発電の海面温度7度上昇は環境に影響皆無と騙しており、これも騙しが明白で海面温度7度上昇を100年続け、原子力発電でCO2排出量を低減しても、海水表面温度7度上昇海域が10%成長で1000倍を超えるため、旱魃や豪雨や風速を10倍の300m/秒台風や季節風として南極の氷を0に近付け、陸と海の食糧が0に近付き、人類が絶滅する背景があります。火力原子力発電では海面温度7度上昇は環境に影響皆無と騙しており、日本近海の海藻類や魚類が絶滅に近付くテレビ報道が実際です。IPCC北極予測も海面温度7度上昇がコンピュータ計算外のため、衛星07年観測北極海海氷面積がIPCC第4次報告書の40年後に近い状態で観測された報道があり、IPCC予測全部を大誤報と考えるのが良く、平均的に1度温度上昇しても異状気象は困難で、90%前後が海面温度7度上昇と考えると、100年前後で海面温度2〜3回上昇14〜21度上昇海域が南極に接近し、南極の氷が0に近付き、海面上昇が77mに近付く背景があります。   In order to prevent the invention of the follow-up engine, the existing engine is skillfully deceived as the best engine in high school and university, and when returning to elementary school science and thinking about the best engine, the unit of horsepower and work rate is kg weight m / sec. × Because of speed, it is the best theoretical engine that generates heavy output with heavy materials at high speed. Furthermore, a 7 degree rise in sea surface temperature of thermal nuclear power generation is believed to have no impact on the environment, and this is obvious, even if the sea level temperature rises 7 degrees for 100 years and CO2 emissions are reduced by nuclear power generation, Because the sea area where the temperature rises by 7 degrees exceeds 1000 times by 10% growth, Antarctic ice is brought close to 0 as a 300m / second typhoon or seasonal wind that is 10 times higher than drought, heavy rain, and wind speed, and land and sea food approaches 0, There is a background to the extinction of mankind. With thermal nuclear power generation, a 7-degree rise in sea surface temperature is said to have no impact on the environment, and TV reports that seaweeds and fish near Japan are nearing extinction are actual. In the IPCC Arctic prediction, since the sea surface temperature rise of 7 degrees is out of the computer calculation, there is a report that the Arctic sea ice area observed in 2007 was close to 40 years after the IPCC Fourth Report. It is good to think of it as a big misinformation, and even if the temperature rises by 1 degree on average, abnormal weather is difficult, and if about 90% thinks that the sea surface temperature will rise by 7 degrees, the sea surface temperature will rise 2-3 times around 100 years 14 ~ There is a background in which the sea area rising 21 degrees approaches the South Pole, the Antarctic ice approaches 0, and the sea level rise approaches 77m.

馬力や仕事率の単位がkg重m/秒等重量×速度のため、重い物質を重力加速度加速にして回転出力を発生するのが理論最良エンジンですが、考えた痕跡が皆無という背景があります。そこで消費燃料僅少の竪型全動翼液体金属太陽熱エンジン駆動飛行機類や船舶類にして、停止中は熱と電気と冷熱の供給設備で使用可能に地球温暖化防止する等とし、大気圧同速度同容積仕事率kg重m/秒を既存蒸気タービンの1〜2.3万倍液体金属仕事率にして、水銀・液体鉛・液体ビスマス・液体錫・液体カドミウム・液体インジウム・液体ガリウム・液体亜鉛・液体タリウム等液体金属を垂直下方に重力加速度加速にすると、低速で落差を増大する入力より重力加速度加速だけでも出力発生は大幅に増大し、タービンの大型化多数化+落差を1000m以上に増大限り無く出力を増大できる背景があります。地球での最大加速が重力加速度で無限大に近く、海水温度上昇0やCO2排気0や燃料費0の理論最良エンジン重力発電として、化石燃料等限りある資源が枯渇するため、限りある資源を子孫に残す手段の温熱や冷熱の回収利用無限大や無限大に近い発電量とし、重力発電蓄電池駆動や電気駆動の、各種自動車類全盛や各種船舶類全盛や全面電化住宅全盛等、極端に安価な発電の蓄電池駆動や電気駆動の地球温暖化防止が得られる背景があります。   Since the unit of horsepower and power is kg weight m / s, equal weight x speed, the best engine theoretically generates heavy output by accelerating gravitational acceleration, but there is a background that there is no trace of thought. Therefore, it would be possible to use a vertical all-blade liquid metal solar engine driven airplane or ship with a small amount of fuel consumption, and to use it with heat, electricity and cold supply equipment during stoppage to prevent global warming, etc. With the same volumetric power kg weight m / sec 1 to 230,000 times that of the existing steam turbine, the liquid metal work rate is mercury, liquid lead, liquid bismuth, liquid tin, liquid cadmium, liquid indium, liquid gallium, liquid zinc.・ If liquid acceleration such as liquid thallium is accelerated downward in the vertical direction, the output generation will be greatly increased by the acceleration of gravitational acceleration alone rather than the input that increases the head at low speed, increasing the number of turbines and increasing the head to over 1000m. There is a background that can increase the output without limit. Since the maximum acceleration on the earth is almost infinite in terms of gravitational acceleration, and the theoretical best engine gravity power generation with zero seawater temperature rise, zero CO2 exhaust, and zero fuel cost, fossil fuels and other limited resources are depleted, so limited resources are descended Recovering and using heat and cold as the means to leave the power generation amount is infinite or nearly infinite, and it is extremely inexpensive, such as gravitational power storage battery drive and electric drive, various types of automobiles, various types of ships, and full-scale electrified houses There is a background that can be used to prevent global warming by driving electric storage batteries and driving electricity.

外れて欲しい予想は、中国が10%成長を50年続けると海水温度上昇量が現在の32倍になり、日本の季節風が50〜80m/秒となって国土全部が海水に汚染され、農業と緑が壊滅して餓死者続出が類似世界に拡大する可能性があり、今の雇用不安も小泉総理に再三予想を提供の日本大企業80%前後ゴーストタウン化が始まったのではと心配、危機をチャンスにする知恵が必要です。昭和17〜18年に理論最良エンジンの発明を決意実際は改良から始め、昭和38年岡山地方発明センターの請負で試作を開始して、自分でも試作を続けましたがエンジンの試作は非常に困難です。そこで昭和57年2月より国内大企業等多数にご協力のお願い始めましたが、日本企業等の協力が皆無で、外国唯一お願いしたクリントン大統領の協力がお願いの都度3年3回得られ、1992年米国特許5133305号、1993年米国特許5230307号、1995年米国特許5429078号の駄目発明が判明したのです。既存のエンジンに致命的な欠点が非常に多く改良発明不可能が判明し、急がば回れと1997年ホームページを開設して欠点を1つ改良特許出願して、2008年理論最良エンジンに到達し、元大統領の協力により例えば重力太陽熱発電により燃料費0で発電機及び熱ポンプを駆動して、無限大に近い電気及び温熱と冷熱を極端に安価製造タービン駆動可能とし、500°C以下液体金属発電で、大気圧同速度同容積仕事率を既存蒸気タービン発電の1〜2.3万倍にして、実際に実験して実験最良エンジンに移行したいのです。   The expectation is that if China continues to grow at 10% for 50 years, the rise in seawater temperature will be 32 times the current level, and the Japanese seasonal wind will be 50-80 m / sec. Concerns about the start of ghost towns around 80% of large Japanese companies that provide the prospect of Prime Minister Koizumi again with the fear that employment will continue to spread to a similar world due to the destruction of greenery. We need wisdom to make a chance. Decided to invent the theoretical best engine in 1958 and 1980. Actually started with improvements, started the prototype at the Okayama Regional Invention Center in 1963, and continued to make the prototype myself, but the engine prototype was very difficult. . Therefore, in February 1982, we started requesting cooperation from a large number of domestic large corporations, etc., but there was no cooperation from Japanese companies, etc., and every time we asked for the cooperation of President Clinton, the only request from foreign countries, three times a year, The 1992 US Patent 5133305, 1993 US Patent 5230307, and 1995 US Patent 5429078 were found to be useless. There were so many fatal faults in the existing engine that it was impossible to improve the invention. In a hurry, the 1997 homepage was opened, and a patent for improving one fault was filed. With the cooperation of the former president, for example, gravitational solar power generation can drive generators and heat pumps at zero fuel cost, making it possible to drive nearly infinite electricity, heat and cold at an extremely inexpensive manufacturing turbine, and liquid metal below 500 ° C With power generation, I want to make the atmospheric pressure, the same speed, and the same volumetric power of 1 to 23,000 times that of the existing steam turbine power generation, and actually experiment and move to the best experimental engine.

米国特許第6119650号、中国特許第8818号、EU英国特許902175号、米国特許第6263664号があり、上記多数の背景技術を改良や、下記特許文献2も理論最良エンジン発明の過程の発明や、実験最良を狙う発明では、液体金属重力発電で蒸気タービン発電の1〜2.3万倍発電にする実験をしよう、太陽熱を種に重力駆動熱ポンプで無限大に近い温熱と冷熱製造の実験をしよう、液体金属重力発電で既存世界の10倍発電量にしよう、化石燃料等限りある資源の燃焼は必要最小限にして子孫に残そう、等があります。There are US Pat. No. 6,119,650, Chinese Patent No. 8818, EU British Patent No. 902175, US Pat. No. 6,263,664, and many of the above-mentioned background technologies have been improved. In the invention aiming at the best experiment, let's experiment to make liquid metal gravity power generation 1 to 23,000 times that of steam turbine power generation, using solar heat as a seed, experiment of warm and cold production near infinity with gravity driven heat pump Let's make liquid metal gravity power generation 10 times as much as the existing world, fossil fuels and other limited resources to burn to the next generation with the minimum necessary.

先の出願として特願2007−179204号、特願2007−221970号、特願2007−237367号、特願2007−250348号、特願2007−265115号、特願2008−6612号、特願2008−22246号、特願2008−24656号、特願2008−28582号、特願2008−30162号、特願2008−94452号、特願2008−99870号、特願2008−125665号、特願2008−134046号、特願2008−137629号、特願2008−157556号、特願2008−158830号、特願2008−162842号、特願2008−164111号、特願2008−166907号、特願2008−169979号、特願2008−173046号、特願2008−174231号、特願2008−178700号、特願2008−179872号、特願2008−181052号、特願2008−182325号、特願2008−186795号、特願2008−188165号、特願2008−202677号、特願2008−203842号、特願2008−206632号、特願2008−209497号、特願2008−214912号、特願2008−229434号、特願2008−231842号、特願2008−243690号、特願2008−245061号、特願2008−249719号、特願2008−256006号、特願2008−266020号、特願2008−269294号、特願2008−282825号、特願2008−288411号、特願2008−290630号、特願2008−295174号、特願2008−299091号、特願2008−305951号、特願2008−319210、特願2008−327045号と、実験最良を狙う特願2009−011656号、特願2009−013856号、特願2009−015027号、特願2009−016249号、特願2009−021161号、特願2009−022247号、特願2009−023345号、特願2009−024512号、特願2009−025684号、特願2009−026989号、特願2009−028105号、特願2009−028150号、特願2009−028253号、特願2009−029406号、特願2009−029471号、特願2009−029539号、特願2009−030759号、特願2009−030865号、特願2009−030942号、特願2009−032264号、特願2009−032312号、特願2009−032378号、特願2009−033490号、特願2009−033534号、特願2009−033679号、特願2009−037263号、特願2009−048869号、特願2009−048951号、特願2009−049078号、特願2009−057455号、特願2009−057586号、特願2009−057745号、特願2009−077911号、特願2009−078042号があります。As prior applications, Japanese Patent Application No. 2007-179204, Japanese Patent Application No. 2007-221970, Japanese Patent Application No. 2007-237367, Japanese Patent Application No. 2007-250348, Japanese Patent Application No. 2007-265115, Japanese Patent Application No. 2008-6612, and Japanese Patent Application No. 2008- No. 22246, Japanese Patent Application No. 2008-24656, Japanese Patent Application No. 2008-28582, Japanese Patent Application No. 2008-30162, Japanese Patent Application No. 2008-94452, Japanese Patent Application No. 2008-99870, Japanese Patent Application No. 2008-125665, Japanese Patent Application No. 2008-134046. No., Japanese Patent Application No. 2008-137629, Japanese Patent Application No. 2008-157556, Japanese Patent Application No. 2008-158830, Japanese Patent Application No. 2008-162842, Japanese Patent Application No. 2008-164111, Japanese Patent Application No. 2008-166907, Japanese Patent Application No. 2008-169799. Japanese Patent Application No. 2008-173046, Japanese Patent Application No. 20 Japanese Patent Application No. 8-174231, Japanese Patent Application No. 2008-178700, Japanese Patent Application No. 2008-179882, Japanese Patent Application No. 2008-181052, Japanese Patent Application No. 2008-182325, Japanese Patent Application No. 2008-186895, Japanese Patent Application No. 2008-188165, Japanese Patent Application No. 2008. No. -202676, Japanese Patent Application No. 2008-203842, Japanese Patent Application No. 2008-206632, Japanese Patent Application No. 2008-209497, Japanese Patent Application No. 2008-214912, Japanese Patent Application No. 2008-229434, Japanese Patent Application No. 2008-231842, Japanese Patent Application No. 2008- No. 243690, Japanese Patent Application No. 2008-244501, Japanese Patent Application No. 2008-249719, Japanese Patent Application No. 2008-256006, Japanese Patent Application No. 2008-266020, Japanese Patent Application No. 2008-269294, Japanese Patent Application No. 2008-282825, Japanese Patent Application No. 2008-288411 No., Japanese Patent Application 2008- No. 90630, Japanese Patent Application No. 2008-295174, Japanese Patent Application No. 2008-290991, Japanese Patent Application No. 2008-305951, Japanese Patent Application No. 2008-319210, Japanese Patent Application No. 2008-327045, Japanese Patent Application No. 2009-011656, Japanese Patent Application No. 2009-011656, No. 2009-013856, No. 2009-015027, No. 2009-016249, No. 2009-021161, No. 2009-022247, No. 2009-023345, No. 2009-024512, No. 2009-024512 2009-025684, Japanese Patent Application No. 2009-026989, Japanese Patent Application No. 2009-028105, Japanese Patent Application No. 2009-028150, Japanese Patent Application No. 2009-028253, Japanese Patent Application No. 2009-029406, Japanese Patent Application No. 2009-029471, Japanese Patent Application No. 2009 -029539, Japanese Patent Application No. 20 09-030759, Japanese Patent Application No. 2009-030865, Japanese Patent Application No. 2009-030942, Japanese Patent Application No. 2009-032264, Japanese Patent Application No. 2009-032312, Japanese Patent Application No. 2009-032378, Japanese Patent Application No. 2009-033490, Japanese Patent Application No. 2009 No. -035344, Japanese Patent Application No. 2009-033679, Japanese Patent Application No. 2009-037263, Japanese Patent Application No. 2009-048869, Japanese Patent Application No. 2009-049551, Japanese Patent Application No. 2009-049078, Japanese Patent Application No. 2009-057455, Japanese Patent Application No. 2009- No. 057586, Japanese Patent Application No. 2009-057745, Japanese Patent Application No. 2009-077911, and Japanese Patent Application No. 2009-078042.

既存世界の火力原子力発電所では、CO2増大地球温暖化加速や海水表面温度摂氏7度上昇海域を100年で1000倍等とし、冬場に海面冷却海底に栄養分を供給していた自然現象を不可能として、植物プランクトンや海草類やサンゴ等を激減、食物連鎖により魚類の食糧激減魚類を大幅に激減人類の海中食物を限り無く減少し、旱魃や集中豪雨や台風や季節風を100年で10倍等に増大して、例えば台風や季節風を300m/秒等として陸上での食糧生産も加速度的に困難とし、人類絶滅の危険を増大のため、地球温暖化防止して人類絶滅を先送りする課題が在り、化石燃料を大量に燃焼すると地球が温暖化すると共に資源が枯渇するため、空気抵抗0の宇宙利用全盛の飛行機類や船舶類にして、化石燃料燃焼は必要最少にし、限りある資源を子孫に残すと共に、CO2排気僅少や海水温度上昇0にする課題があります。   In the existing world thermal power plants, CO2 increases global warming acceleration and sea surface temperature rises 7 degrees Celsius by 1000 times in 100 years, and the natural phenomenon that supplies nutrients to the sea surface cooling seabed in winter is impossible As a result, phytoplankton, seaweeds, corals, etc. are drastically reduced, fish foods are drastically reduced by the food chain, and humans' marine foods are drastically reduced. Increasing, for example, typhoons and seasonal winds at 300m / s, etc., make it difficult to produce food on land at an accelerated rate, and to increase the danger of human extinction, there is a challenge to prevent global warming and postpone human extinction, Combustion of fossil fuels will cause global warming and depletion of resources. For this reason, fossil fuel combustion will be minimized and limited to space-based airplanes and ships with zero air resistance. Along with leaving the resources in the offspring, there are challenges in CO2 exhaust insignificant or sea water temperature rise 0.

熱製造の熱ポンプを液体金属太陽熱タービンで駆動すると、温熱(過熱蒸気熱量等)と冷熱(圧縮空気質量等)を燃料費0で無限製造の挑戦となり、重力太陽熱発電や重力太陽エンジンにより、太陽熱や熱製造装置の熱ポンプにより温熱と冷熱の製造量を無限大に近付け、限りある石油資源等はCO2にせず大切な資源として必要最小限の使用とし、子子孫孫まで残すと共に地球温暖化防止して、旱魃や海面上昇や台風や季節風の巨大化を阻止し、海底に冷熱の酸素や窒素等の栄養分を供給して、植物プランクトンや海草類やサンゴや魚類等を増殖人類の食物を増大し、既存世界の10倍発電量以上として、既存世界の火力原子力発電所を全廃重力発電にし、重力発電の蓄電池駆動各種自動車類全盛や、蓄電池駆動各種船舶類全盛や電気駆動全面電化住宅全盛や工場電化全盛や温熱と冷熱利用全盛にして、海水温度上昇0やCO2排気0や燃料費0で発電し、地球温暖化防止して人類絶滅を先送りして、重力太陽熱タービンで温熱(圧縮空気熱量圧力)や冷熱(圧縮空気質量圧力)の製造を無限に継続し、温熱を過熱蒸気50で保存短時間最大熱量噴射推進出力を可能として、宇宙上昇時にはスクラムジェットと合体した合体機関噴射部78Sにより短時間噴射推進力を、既存ジェット機の100倍圧力10倍熱量噴射1000倍噴射出力狙いとし、飛行機類や船舶類も燃料消費が0に近い宇宙利用全盛にして、宇宙飛行時にも燃料消費0で過熱蒸気を製造し、燃料消費僅少で限りある資源を子孫に残します。 When a heat pump for heat production is driven by a liquid metal solar turbine, heat (superheated steam heat, etc.) and cold heat (compressed air mass, etc.) become a challenge for infinite production with zero fuel cost. And heat production equipment heat pumps to bring the production of hot and cold heat to infinity, and limited oil resources, etc. are not required for CO2 and are used as the minimum necessary resources, leaving them to descendants and preventing global warming In this way, drought, sea level rise, typhoon and seasonal winds are prevented from growing, and nutrients such as cold oxygen and nitrogen are supplied to the sea floor to increase phytoplankton, seaweeds, corals and fish, etc. The existing world's thermal nuclear power plants will be completely abolished by gravitational power generation, and the power generation of various batteries driven by batteries, the power of various batteries driven by ships, and electric drive Surface electric house prime, factory electrification prime, hot and cold use prime, generate seawater temperature rise 0, CO2 exhaust 0 and fuel cost 0, prevent global warming and postpone human extinction, with gravity solar heat turbine Production of warm heat (compressed air calorie pressure) and cold heat (compressed air mass pressure) is continued infinitely, the heat is stored with superheated steam 50, and the maximum calorie injection propulsion output is possible for a short time. The engine injection unit 78S aims to provide a short-time injection propulsion force that is 100 times the pressure of existing jets, 10 times the amount of heat, and 1000 times the fuel injection output. Will produce superheated steam with zero fuel consumption, leaving a limited amount of resources for its offspring.

CO2排気僅少燃料消費僅少の竪型全動翼液体金属太陽熱タービン8G複数駆動を、熱量タービン駆動と質量タービン駆動とし、宇宙では熱量駆動と質量駆動に大気中では重力追加駆動で使用して、液体金属太陽熱エンジン回転出力発生にし、噴射推進出力を既存ジェット機の100倍圧力10倍熱量噴射短時間1000倍噴射推進出力狙いとして、複数の竪型全動翼液体金属太陽熱タービン8G駆動の液体金属太陽熱エンジンとし、宇宙では太陽光直射部120度Cと日陰部−150度Cという絶好環境を利用して、過熱蒸気タービン駆動や過熱蒸気製造絶好の環境を利用して、吸入空気路を密閉空気路として圧縮空気減圧して120度太陽光を長レンズ等で回収し、過熱蒸気でタービン駆動熱ポンプにより1200度前後に圧縮空気を圧縮熱交換過熱蒸気製造にして、タービン排気を−150度日陰部で冷却して復水にする循環を繰り返し、通常は燃焼ガス使用0合体機関噴射部79Kより過熱蒸気50のみ噴射する噴射推進出力発生にして、燃料量0で既存ジェットエンジンの10倍噴射推進出力狙いにし、燃料消費僅少として既存世界の各種船舶類や各種飛行機類で宇宙利用全盛を狙う効果と、資源を子孫に残す効果があります。   CO2 exhaust gas fuel consumption is small vertical all-blade liquid metal solar thermal turbine 8G multiple drive, calorie turbine drive and mass turbine drive in space, heat drive and mass drive in the atmosphere with gravity additional drive in the atmosphere, liquid A liquid solar power engine driven by a plurality of vertical all-blade liquid metal solar turbines 8G with the aim of generating a rotary output of the metal solar engine and aiming at a jet propulsion output of 100 times the pressure of existing jets, 10 times the amount of heat injection, and 1000 times the time of the propulsion output. In space, the intake air passage is used as a sealed air passage by using a superheated steam turbine drive or superheated steam production environment using a perfect environment of sunlight directing part 120 degrees C and shade part -150 degrees C Compressed air is depressurized and 120-degree sunlight is collected with a long lens. Heat exchange superheated steam production, turbine exhaust is cooled in the shaded part of -150 ° C and recirculated to repeat condensate, and usually the combustion propulsion output is generated by injecting only superheated steam 50 from the combined gas injection unit 79K using combustion gas As a result, it has the effect of aiming at 10 times the injection propulsion output of the existing jet engine with the fuel amount of 0, aiming to make the best use of space in various ships and airplanes in the existing world with little fuel consumption, and the effect of leaving resources to the offspring .

熱量駆動竪型全動翼液体金属太陽熱タービン8Gの説明図(実施例1)Explanatory drawing of a calorie-driven vertical all blade liquid metal solar thermal turbine 8G (Example 1) 質量駆動竪型全動翼液体金属太陽熱タービン8Gの説明図(実施例2)Explanatory drawing of mass drive vertical type moving blade liquid metal solar thermal turbine 8G (Example 2) 液体金属重力太陽熱宇宙往還機39Aの説明図(実施例3)Explanatory drawing of liquid metal gravity solar thermal spacecraft 39A (Example 3) 液体金属重力太陽熱宇宙往還飛行船舶39Gの説明図(実施例4)Explanatory drawing of 39G of liquid metal gravity solar thermal space return flight ship (Example 4) 合体機関噴射部78Sの説明図(実施例5)Explanatory drawing of the union engine injection part 78S (Example 5)

発明の実施の形態や実施例を、図面を参照して説明するが、実施形態や実施例と既説明とその構成が略同じ部分には、同一の名称又は符号を付して、重複説明はできるだけ省略し、特徴的な部分や説明不足部分は、順次追加重複説明する。又非常に難解な脳内理論最良エンジン発明のためと、意図する所及び予想を具体的に明快に説明するため、アイディアを仮説数字で説明するが、正解は実験数字として理論最良エンジンの仮説数字に限定しません。最良と思われるアイディアを多数の用途で重複説明し、用途に合せてアイディアを選択使用して、請求項では多用途に合せて選択使用するため千変万化し、理論最良エンジンから順次噴射推進を含めた実験最良エンジンに移行実用化します。   Embodiments and examples of the invention will be described with reference to the drawings, but the same names or reference numerals are given to portions that are substantially the same as those of the embodiments and examples and the description, and redundant description will be omitted. Omitted as much as possible, and the characteristic part and the lack of explanation will be explained in duplicate. The idea is explained with hypothetical figures for the very difficult brain theory best engine invention and to clearly explain the intended place and expectation, but the correct answer is the hypothetical figure of the theoretical best engine as an experimental figure. It is not limited to. The idea that seems to be the best is duplicated in many applications, the idea is selected and used according to the application, and the claims are changed to be used according to the various applications. Transition to the best engine for practical use.

図1の熱量駆動竪型全動翼液体金属太陽熱タービン8Gでは、断熱保温角型タービン外箱77aを正方形に近付け、角部に保温装置付増大球上昇装置2Fを設けて、圧縮熱回収器2Cや電気で温度管理された合金を含む液体金属を最上部に上昇保存して、外箱77a内に1〜10段等タービンを垂直に多段に設けて用途に合わせた台数使用にし、液体金属噴射ポンプ6Lで400MPa等噴射圧縮空気熱量加速重力加速度加速して、竪型全動翼液体金属太陽熱タービン8Gを駆動し、保温タービン間に横軸1hを設け、角型タービン外箱77a外で発電機1や熱製造装置の熱ポンプ1G多数を駆動して、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、太陽熱を種に熱ポンプ1Gと空気熱交換器2Xで無限大に近い温熱(圧縮空気熱量の過熱蒸気)や冷熱(圧縮空気質量)を製造して、宇宙上昇時には横軸1h圧縮熱回収器2C燃料噴射燃焼限り無く高圧燃焼熱交換冷却燃焼し、既存ジェット機の10〜100倍圧力等で図5図6合体機関噴射部78S78Tに供給して、燃料噴射燃焼外周の過熱蒸気50を加熱全量で10倍熱量等を噴射し、図3図4噴射推進出力を既存ジェット機の100〜1000倍に短時間近付け、宇宙到達時には120度太陽光を密閉空気路長レンズと減圧排気圧縮空気で回収して、熱ポンプで1200度前後に圧縮熱交換冷却過熱蒸気50を製造飛行準備するエンジンにします。   In the calorie-driven vertical all-blade liquid metal solar thermal turbine 8G of FIG. 1, the heat insulating and retaining rectangular turbine outer casing 77a is brought close to a square, and the increased sphere raising device 2F with a heat retaining device is provided at the corner, thereby compressing the heat recovery unit 2C. Liquid metal containing an alloy whose temperature is controlled by heat and electricity is stored at the top, and turbines such as 1 to 10 stages are arranged vertically in multiple stages in the outer box 77a so that the number of liquids can be used according to the application. Pump 6L, etc., 400MPa, etc. Compressed compressed air calorie acceleration Acceleration of gravitational acceleration to drive vertical all blade liquid metal solar thermal turbine 8G, horizontal axis 1h is provided between heat retaining turbines, generator outside square turbine outer box 77a 1 and many heat pumps 1G of the heat production apparatus are driven, the rotation direction of the turbine 8G is alternated so that vibrations and noises are negligibly reduced, and the heat pump 1G and the air heat exchanger 2X are nearly infinite by using solar heat as seeds. Heat (pressure) Superheated steam with air calorie) and cold (compressed air mass) are produced, and when the space rises, the horizontal axis 1h compression heat recovery unit 2C fuel injection combustion without limit high-pressure combustion heat exchange cooling combustion, 10 to 100 times the pressure of existing jets 5 is supplied to the combined engine injection unit 78S78T in FIG. 5, and the superheated steam 50 on the outer periphery of the fuel injection combustion is injected 10 times as much as the total amount of heating, and FIG. When it reaches space, 120 degree sunlight is collected with a sealed air path length lens and decompressed exhaust compressed air, and a heat pump is used to make a compressed flight heat-cooled superheated steam 50 around 1200 degrees with a heat pump. The

宇宙到達過熱蒸気を製造の熱量駆動液体金属太陽熱タービン8G排気の過程では、宇宙日陰部−150度Cで排気を冷却復水にし、圧縮熱回収器2Cで過熱蒸気50にして、竪型全動翼液体金属太陽熱タービン8Gを過熱蒸気50熱量駆動する宇宙使用にし、内側動翼群60C外側動翼群60Dは、可能な限り全自動加工可能に段落毎同径略同形として嵌合ボルト組立にして、多段動翼群と多段タービンを可能にすると共に全自動加工や組立容易にし、液体金属を加速する重力加速部1gには発電機1や熱ポンプ1Gを駆動する横軸1h貫通穴を具備して、発電機1や熱ポンプ1Gを断熱保温した角型タービン外箱77aの外で直角駆動し、太陽光加熱の空気を圧縮800〜1200度にして、空気熱交換器2Xで別空気を500度C等に加熱して圧縮800〜1200度にし、繰り返して高圧の圧縮空気28aと過熱蒸気50の製造量を増大して、例えば200度前後24〜400MPa圧縮空気28a質量+400度前後24〜400MPa過熱蒸気50に分割保存し、合金を含む液体金属噴射ポンプ6Lの噴射速度を過熱蒸気50加速重力加速度加速で駆動して、大気圧同速度同容積仕事率kg重m/秒を既存蒸気タービンの1〜2.3万倍にし、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射して、転がり接触回転出力発生とし、排気の過程では水復水器2a冷熱(質量タービン排気を含む)復水器2Hと空気抽出器51で真空にして、圧縮空気質量製造と熱量(過熱蒸気)を製造する、海水温度上昇0CO2排気0の熱量駆動液体金属太陽熱タービンにします。 In the process of exhausting the superheated steam reaching the space, the exhaust gas is cooled and condensed at a space shade of 150 ° C, and the superheated steam 50 is converted into a superheated steam 50 by the heat recovery unit 2C. The blade liquid metal solar thermal turbine 8G is used in space to drive 50 superheated steam, and the inner rotor blade group 60C and outer rotor blade group 60D can be fully automated as much as possible, and can be assembled into a fitting bolt assembly with the same diameter and shape of each paragraph. The gravitational acceleration unit 1g for accelerating the liquid metal has a horizontal shaft 1h through-hole for driving the generator 1 and the heat pump 1G, enabling a multi-stage rotor blade group and a multi-stage turbine and facilitating fully automatic processing and assembly. Then, the generator 1 and the heat pump 1G are driven at right angles outside the rectangular turbine outer box 77a that is insulated and heat-insulated, the solar heating air is compressed to 800 to 1200 degrees, and another air is supplied by the air heat exchanger 2X to 500 degrees. In addition to degree C etc. Then, the compression amount is set to 800 to 1200 degrees, and the production amount of the high-pressure compressed air 28a and the superheated steam 50 is repeatedly increased, and divided into, for example, a mass of 24-200 MPa compressed air 28a around 200 degrees + a 24-400 MPa superheated steam 50 around 400 degrees. The liquid metal injection pump 6L containing the alloy is driven and driven by the superheated steam 50 acceleration gravity acceleration acceleration, and the atmospheric pressure, the same speed, and the same volumetric power kg weight m / second are 1 to 2.3 of the existing steam turbine. Injected into the turbine blade cross section 4X, which has a cross-sectional area of 2 to 26 times the existing turbine blade cross-sectional area to generate rolling contact rotation output, and in the exhaust process, water condenser 2a cold (including mass turbine exhaust) ) Vacuum generated by condenser 2H and air extractor 51 to produce mass of compressed air and produce calorie (superheated steam), seawater temperature rise 0CO2 exhaust 0 calorie drive liquid metal solar heat And the turbine.

図2の竪型全動翼液体金属太陽熱タービン8G質量駆動でも、断熱保温角型タービン外箱77aを正方形に近付け、角部に保温装置付増大球上昇装置2Fを設けて、圧縮熱回収器2Cや電気で温度管理された合金を含む液体金属を最上部に上昇保存して、外箱77a内に1〜10段等タービンを垂直に多段に設けて用途に合わせた台数使用にし、液体金属噴射ポンプ6Lで400MPa等噴射し圧縮空気質量加速重力加速度加速して、竪型全動翼液体金属太陽熱タービン8Gを駆動し、保温タービン間重力加速部1gに貫通穴と横軸1hを設け、角型タービン外箱77a外で発電機1や熱製造+圧縮空気製造の、熱ポンプ1G多数駆動の圧縮熱回収器2C空気熱交換器2X水熱交換器2Yにして、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、質量タービン駆動膨張して絶対0度に近付く圧縮空気を液体金属で加熱噴射出力増大して、減圧低圧低温圧縮空気28aを熱回収最適媒体にし、宇宙到達時には120度太陽光熱量を密閉吸入空気路28Aを利用熱回収して、500度前後を熱ポンプ1Gで圧縮1200度前後にし、圧縮熱回収器2Cで熱交換過熱蒸気50を製造繰り返し熱回収500度前後にして、宇宙では過熱蒸気50を製造貯蔵する質量駆動のタービンにします。 In the vertical all-blade liquid metal solar turbine 8G mass drive of FIG. 2, the heat insulating and retaining angular turbine outer casing 77a is brought close to a square, and the increased sphere raising device 2F with a heat retaining device is provided at the corner, and the compression heat recovery device 2C Liquid metal containing an alloy whose temperature is controlled by heat and electricity is stored at the top, and turbines such as 1 to 10 stages are arranged vertically in multiple stages in the outer box 77a so that the number of liquids can be used according to the application. The pump 6L injects 400MPa and the like, accelerates the compressed air mass acceleration gravity acceleration, drives the vertical all-blade liquid metal solar thermal turbine 8G, and provides a through hole and a horizontal axis 1h in the thermal acceleration turbine inter-gravity acceleration portion 1g. Outside the turbine outer box 77a, the generator 1 and heat production + compressed air production heat pump 1G compression drive heat recovery unit 2C air heat exchanger 2X water heat exchanger 2Y, the turbine 8G rotating direction alternately Vibration and The noise is canceled out little, and the compressed air that approaches mass turbine drive expansion and approaches absolute 0 degree is heated and injected with liquid metal. The reduced pressure, low pressure and low temperature compressed air 28a is used as the optimum heat recovery medium. The amount of heat is recovered by using the sealed intake air passage 28A, and about 500 degrees is compressed by the heat pump 1G to about 1200 degrees, and the heat exchange superheated steam 50 is repeatedly manufactured by the compression heat recovery unit 2C, and the heat recovery is about 500 degrees. In space, it is a mass-driven turbine that produces and stores superheated steam 50.

質量駆動竪型全動翼液体金属太陽熱タービン8Gの、内側動翼群60C外側動翼群60Dは、可能な限り全自動加工可能に段落毎同径略同形として嵌合ボルト組立にして、多段動翼群と多段タービンを可能にすると共に全自動加工や組立容易にし、重力加速部1gには発電機1や熱ポンプ1Gを駆動する横軸1h貫通穴を具備し、大気中を飛行時には前記同様に限り無く高圧の圧縮空気28aと過熱蒸気50の製造量を増大して、例えば200度前後24〜400MPa圧縮空気28a質量+400度前後24〜400MPa過熱蒸気50に分割保存し、圧縮空気28a質量の一部で質量タービン駆動大部分を噴射推進に使用して、質量駆動竪型全動翼液体金属太陽熱タービン8Gは、合金を含む液体金属噴射ポンプ6Lの噴射速度を圧縮空気質量加速と重力加速度加速で駆動し、大気圧同速度同容積仕事率kg重m/秒を既存蒸気タービンの1〜2.3万倍にして、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射し、転がり接触回転出力発生として、大気中排気の過程では水復水器2a+冷熱復水器2H+空気抽出器51+放出から選択で低圧空気排気にし、燃料費0液体金属の熱量質量駆動タービンで圧縮空気製造と熱製造する、海水温度上昇0CO2排気0の液体金属重力質量タービンにします。 The inner rotor blade group 60C and outer rotor blade group 60D of the mass-driven vertical all-blade liquid metal solar thermal turbine 8G can be fully automatically processed as much as possible by making fitting bolts assembling bolts with the same diameter and the same shape for each stage. Enables blade group and multi-stage turbine and facilitates fully automatic machining and assembly. Gravity accelerating unit 1g is provided with a horizontal shaft 1h through hole for driving generator 1 and heat pump 1G. The production amount of high-pressure compressed air 28a and superheated steam 50 is increased without limitation, and is divided and stored, for example, in a mass of compressed air 28a around 24 to 400 MPa + a mass of compressed air 28a around 400 degrees and a superheated steam 50 of around 400 degrees. Partly using a large part of the mass turbine drive for injection propulsion, the mass driven vertical all blade liquid metal solar thermal turbine 8G compresses the injection speed of the liquid metal injection pump 6L containing the alloy with compressed air Driven by mass acceleration and acceleration of gravitational acceleration, the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec, are 1 to 23,000 times that of the existing steam turbine, and the cross-sectional area is 2 to 26 times that of the existing turbine blade. Injected into the turbine blade cross section 4X, the rolling contact rotation output is generated, and in the process of exhaust in the atmosphere, the water condenser 2a + cold condenser 2H + air extractor 51 + release is selected as low-pressure air exhaust, and the fuel cost is 0 liquid It is a liquid metal gravity mass turbine with 0CO2 exhaust and 0 seawater temperature rise, which produces compressed air and heat with a metal calorie mass driven turbine.

図3の液体金属重力太陽熱宇宙往還機39A噴射推進出力発生では、重力使用が限定されるため飛行胴38a垂直翼38dを一体として、複数竪型全動翼液体金属太陽熱タービン8G台数選択使用で落差を最適にし、翼前縁心38e空気吸入口28Bより空気28aを吸入の過程で、長レンズ2d熱吸収材2Bで構成の吸入空気路28Aで太陽熱加熱の空気28aを吸入して、複数タービン駆動の熱ポンプ1Gで圧縮800〜1200度にし、空気熱交換器2Xの別空気28a熱回収熱ポンプ1Gで圧縮熱回収を繰り返す熱製造として、宇宙上昇時には圧縮熱回収器2Cで燃料噴射燃焼限り無く高圧燃焼熱交換冷却燃焼し、繰り返し圧縮800〜1200度にして水熱交換器2Yで熱回収を繰り返して、過熱蒸気50と燃焼ガス49質量を既存ジェット機噴射圧力の10〜100倍圧力等で合体機関噴射部79Kに供給し、燃料噴射燃焼外周の過熱蒸気50を加熱全部で10倍熱量等を噴射して、噴射推進出力を既存ジェット機の100〜1000倍に短時間近付け、宇宙では超音速マッハ32の地球脱出速度や光の速度に近付ける、各種宇宙往還機39A類や各種航空機類で燃料費0に近い宇宙利用全盛にし、大気中を通常飛行時には既存ジェット機の10〜100倍圧力1/10熱量過熱蒸気50噴射等として、圧縮空気28a質量と過熱蒸気50を貯蔵増大します。   In the generation of jet propulsion output of the liquid metal gravity solar space return aircraft 39A in FIG. 3, the use of gravity is limited. In the process of sucking air 28a from the air inlet 28B of the blade leading edge 38e, solar-heated air 28a is sucked in the intake air passage 28A composed of the long lens 2d heat absorbing material 2B, and a plurality of turbines are driven. The heat pump 1G compresses 800 to 1200 degrees, and heat production repeats the recovery of compression heat with the separate air 28a heat recovery heat pump 1G of the air heat exchanger 2X. High-pressure combustion heat exchange cooling combustion, repeatedly compression 800-1200 degrees, repeated heat recovery in the water heat exchanger 2Y, superheated steam 50 and 49 mass of combustion gas is already The combined injection unit 79K is supplied to the combined engine injection unit 79K at a pressure 10 to 100 times the jet injection pressure, and the superheated steam 50 on the fuel injection combustion outer periphery is heated to inject a total of 10 times the amount of heat, etc. Nearly 1000 times shorter, in space, close to the speed of the supersonic Mach 32's earth escape and the speed of light Occasionally, the mass of compressed air 28a and superheated steam 50 are increased and stored as 10 to 100 times pressure 1/10 calorie superheated steam 50 injection of existing jets.

大気中を飛行時には複数の竪型全動翼液体金属太陽熱タービン8G横軸1h駆動の、熱ポンプ1G・圧縮熱回収器2C・空気熱交換機2X・水熱交換器2Yを、横並び又は立て並びとして、用途に合わせた台数を夫々1〜10段に設けて、用途に合わせて落差を増大した出力増大とし、液体金属を液体金属噴射ポンプ6Lで噴射して、分割保存した圧縮空気熱量+圧縮空気質量+真空+重力で加速し、複数の竪型全動翼液体金属太陽熱タービン8Gに噴射して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にし、タービン翼8cに噴射転がり接触駆動回転出力を発生して、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン回転出力の1〜2.3万倍回転出力にし、熱ポンプ多数を駆動して、24〜400MPa過熱蒸気50熱量+24〜400MPa圧縮空気28a質量を限り無く増大し、空気吸引噴射する噴射推進出力の発生は、合体機関噴射部79Kに分割保存した過熱蒸気50を供給噴射等として、既存ジェット機の10〜100倍圧力1/10噴射熱量10倍噴射推進出力大型化等とし、合体機関噴射部79K円筒回転部77Gを180度以上回転して、逆噴射や垂直上昇垂直降下を可能にし、宇宙利用やビルの屋上や月面等何処でも飛行場として着陸可能にします。 When flying in the atmosphere, heat pump 1G, compression heat recovery unit 2C, air heat exchanger 2X, and water heat exchanger 2Y driven by a plurality of vertical all-blade liquid metal solar thermal turbine 8G horizontal shaft 1h are arranged side by side or side by side. The number of units according to the application is provided in 1 to 10 stages, the output is increased by increasing the head according to the application, the liquid metal is injected by the liquid metal injection pump 6L, and the stored compressed air heat amount + compressed air Accelerates by mass + vacuum + gravity, and injects into a plurality of vertical all-blade liquid metal solar thermal turbines 8G, making the turbine blade cross section 4X 2 to 26 times that of existing steam turbines, spraying rolling contact drive rotation on turbine blades 8c Generates output, sets the atmospheric pressure, the same speed, and the same volumetric work rate (kg / m) to 1 to 23,000 times the rotation output of the existing steam turbine, drives many heat pumps, and overheats 24 to 400 MPa. steam 0 heat amount +24 to 400 MPa Compressed air 28a The mass of the compressed air 28a is increased as much as possible, and the generation of injection propulsion output for air suction injection is performed by using superheated steam 50 divided and stored in the combined engine injection unit 79K as supply injection or the like. Double pressure 1/10 injection heat amount 10 times injection propulsion output enlargement, etc. Combined engine injection part 79K cylindrical rotation part 77G is rotated 180 degrees or more to enable reverse injection and vertical ascending vertical descent, space use and building use Make it possible to land as an airfield anywhere on the rooftop or moon.

宇宙到達時には質量駆動竪型全動翼液体金属太陽熱タービン8G駆動の過程で、120度太陽光の熱量を長レンズ2d熱吸収材2Bで熱回収し、吸入空気路28Aを密閉質量駆動タービンの圧縮空気排気により熱回収して、500度前後を熱量駆動と質量駆動のタービンで駆動の多数熱ポンプ1Gで圧縮し、1200度前後にして圧縮熱回収器2Cで熱交換過熱蒸気50を製造繰り返し熱回収500度前後にして、宇宙では過熱蒸気50を製造貯蔵する質量駆動のタービン8Gと熱量駆動のタービン8Gにし、宇宙での噴射推進は過熱蒸気50による噴射推進として、圧縮空気は過熱蒸気50の製造に使用して長距離の宇宙旅行を可能にします。   At the time of reaching the space, in the process of driving the mass-driven vertical all-blade liquid metal solar heat turbine 8G, the heat of 120-degree sunlight is recovered by the long lens 2d heat absorbing material 2B, and the intake air passage 28A is compressed by the sealed mass-driven turbine. Heat is recovered by air exhaust, and is compressed by multiple heat pumps 1G driven by a calorie-driven and mass-driven turbine at around 500 degrees, and heat exchange superheated steam 50 is manufactured repeatedly at about 1200 degrees by the compression heat recovery unit 2C. In the space, the mass-driven turbine 8G that manufactures and stores the superheated steam 50 and the heat-driven turbine 8G are used in the space. Used in manufacturing to enable long distance space travel.

図4の液体金属重力太陽熱宇宙往還飛行船舶39G噴射推進出力発生では、重力使用が限定されるため飛行胴38a垂直翼38dを一体の水面利用船体として、図1図2複数6台等竪型全動翼液体金属太陽熱タービン8G台数選択使用で落差を最適にし、空気吸入口28Bより空気28aを吸入の過程で、長レンズ2d熱吸収材2Bで構成の吸入空気路28Aで太陽熱加熱の空気28aを吸入して、熱ポンプ1Gで圧縮800〜1200度にし、空気熱交換器2Xの別空気28a熱回収熱ポンプ1Gで圧縮熱回収を繰り返す圧縮熱製造として、水熱交換器2Yでは過熱蒸気50製造で熱回収を繰り返す熱製造とし、宇宙上昇時には圧縮熱回収器2Cで液体酸素圧入を含めて燃料噴射燃焼限り無く高圧燃焼熱交換冷却燃焼し、繰り返し圧縮800〜1200度にして水熱交換器2Yで熱回収を繰り返して、過熱蒸気50と燃焼ガス49質量を、既存ジェット機噴射圧力の10〜100倍圧力等で合体機関噴射部79Kに供給し、燃焼ガス49に燃料噴射燃焼外周の過熱蒸気50を加熱全部で10倍熱量等を噴射して、噴射推進出力を既存ジェット機の100〜1000倍に短時間近付け、宇宙では超音速マッハ32の地球脱出速度や光の速度に近付ける、各種宇宙往還飛行船舶39G類や各種航空機類で燃料費0に近い宇宙利用全盛にし、大気中を通常飛行時には噴射熱量を僅少として、圧縮空気28a質量と過熱蒸気50を貯蔵増大します。   Since the use of gravity is limited in the generation of the liquid metal gravity solar thermal space return flight ship 39G jet propulsion output in FIG. 4, the flying body 38a vertical wing 38d is used as an integrated water surface hull, and FIG. By selecting and using the number of moving blade liquid metal solar turbines 8G, the head is optimized, and in the process of sucking the air 28a from the air suction port 28B, the solar heating air 28a is formed in the suction air passage 28A composed of the long lens 2d heat absorbing material 2B. As a compression heat production which is sucked and compressed to 800 to 1200 degrees by the heat pump 1G and the compression heat recovery is repeated by the separate air 28a heat recovery heat pump 1G of the air heat exchanger 2X, the superheated steam 50 is produced by the water heat exchanger 2Y. The heat production is repeated in the heat recovery, and when the space rises, the compression heat recovery unit 2C performs the high pressure combustion heat exchange cooling combustion including the liquid oxygen injection and the repetitive compression 80 The heat recovery is repeated in the water heat exchanger 2Y at ˜1200 degrees, and the superheated steam 50 and the combustion gas 49 mass are supplied to the combined engine injection unit 79K at a pressure 10 to 100 times the existing jet injection pressure, etc. 49, the superheated steam 50 on the outer periphery of the fuel injection combustion is heated up to a total of 10 times the amount of heat, and the injection propulsion output is brought close to 100 to 1000 times that of existing jets in a short time. Various space-returning ships 39G and various aircrafts approaching the speed of light to make the best use of space near the fuel cost of zero, and the amount of compressed air 28a and superheated steam 50 are stored with a small amount of injection heat during normal flight in the atmosphere. Will increase.

大気中を飛行時には複数の竪型全動翼液体金属太陽熱タービン8G横軸1h駆動の、熱ポンプ1G・圧縮熱回収器2C・空気熱交換機2X・水熱交換器2Yを、横並び又は立て並びとして、用途に合わせた台数を夫々1〜10段に設けて、用途に合わせて落差を増大した出力増大とし、液体金属を液体金属噴射ポンプ6Lで噴射して、分割保存した圧縮空気熱量+圧縮空気質量+真空+重力で加速し、複数の竪型全動翼液体金属太陽熱タービン8Gに噴射して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にし、タービン翼8cに噴射転がり接触駆動回転出力を発生して、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン回転出力の1〜2.3万倍回転出力にし、熱ポンプ多数を駆動して、24〜400MPa過熱蒸気50熱量と24〜400MPa圧縮空気28a質量を限り無く増大し、空気吸引噴射する噴射推進出力の発生は、合体機関噴射部79Kに分割保存した過熱蒸気50を供給噴射等として、既存ジェット機の10〜100倍圧力1/10噴射熱量10倍噴射推進出力大型化等とし、回転腕翼7E又は図5円筒回転部77Gを180度以上回転して逆噴射や垂直上昇垂直降下を可能にして、宇宙利用全盛や水上何処でも着水可能にし、月面着陸等の場合は4脚や6却等を設けて着陸可能にします。 When flying in the atmosphere, heat pump 1G, compression heat recovery unit 2C, air heat exchanger 2X, and water heat exchanger 2Y driven by a plurality of vertical all-blade liquid metal solar thermal turbine 8G horizontal shaft 1h are arranged side by side or side by side. The number of units according to the application is provided in 1 to 10 stages, the output is increased by increasing the head according to the application, the liquid metal is injected by the liquid metal injection pump 6L, and the stored compressed air heat amount + compressed air Accelerates by mass + vacuum + gravity, and injects into a plurality of vertical all-blade liquid metal solar thermal turbines 8G, making the turbine blade cross section 4X 2 to 26 times that of existing steam turbines, spraying rolling contact drive rotation on turbine blades 8c Generates output, sets the atmospheric pressure, the same speed, and the same volumetric work rate (kg / m) to 1 to 23,000 times the rotation output of the existing steam turbine, drives many heat pumps, and overheats 24 to 400 MPa. steam The generation of injection propulsion output that increases the amount of 0 heat and 24-400 MPa compressed air 28a without any limit and sucks and injects air is performed by using the superheated steam 50 divided and stored in the combined engine injection unit 79K as supply injection or the like. 100 times pressure 1/10 injection heat amount 10 times injection propulsion output enlargement, etc., rotating arm wing 7E or cylindrical rotating part 77G in FIG. It is possible to land anywhere on the prime or the surface of the water, and in the case of landing on the moon, it is possible to land with 4 legs or 6 rejections.

宇宙到達時には質量駆動竪型全動翼液体金属太陽熱タービン8G駆動の過程で、前記同様に120度太陽光の熱量を長レンズ2d熱吸収材2Bで熱回収し、吸入空気路28Aを密閉質量駆動タービンの圧縮空気排気により熱回収して、500度前後を熱量駆動と質量駆動のタービンで駆動の多数熱ポンプ1Gで圧縮し、1200度前後にして圧縮熱回収器2Cで熱交換過熱蒸気50を製造繰り返し熱回収500度前後にして、宇宙では過熱蒸気50を製造貯蔵する質量駆動のタービン8Gと熱量駆動のタービン8Gにし、宇宙での噴射推進は過熱蒸気50による噴射推進として、圧縮空気は過熱蒸気50の製造に使用して長距離の宇宙旅行を可能にします。   In the process of driving the mass-driven vertical all-blade liquid metal solar thermal turbine 8G when reaching space, heat of 120 degree sunlight is recovered by the long lens 2d heat absorbing material 2B in the same manner as described above, and the intake air passage 28A is sealed and mass-driven. Heat is recovered by the compressed air exhaust of the turbine, and about 500 degrees is compressed by a multiple heat pump 1G driven by a calorie-driven and mass-driven turbine, and the heat exchange superheated steam 50 is generated by the compressed heat recovery unit 2C at about 1200 degrees. Repetitive production heat recovery is around 500 degrees, and in space, the mass-driven turbine 8G that manufactures and stores the superheated steam 50 and the heat-driven turbine 8G are used. Used for the production of steam 50, enabling long-distance space travel.

図5の合体機関噴射部78Sは、過熱蒸気制御弁25を開放して分割保存した過熱蒸気50を燃焼器1Y外周の過熱蒸気溜95cの最上流に供給し、宇宙上昇準備の場合は推進剤の過熱蒸気50製造の過程で圧縮空気28aに燃料噴射燃焼して、圧縮熱回収器2Cで複数回圧縮して燃料噴射燃焼複数回熱回収し、限り無く高圧の燃焼ガス49酸化剤と過熱蒸気50推進剤を貯蔵限り無く増大して、宇宙上昇時には燃焼ガス制御弁24を開放し、200度前後24〜400MPa燃焼ガス49を燃焼ガス溜95a燃焼器1Yの最上流に供給して、燃料制御弁25b開放燃料噴射ポンプ1Dにより燃料1bを燃料噴射ノズル6Xより噴射し、燃焼器1Y最上流で着火燃焼外周の過熱蒸気50を加熱燃焼温度の上昇を可能して、外周長大な過熱蒸気溜95cの400度前後24〜400MPa過熱蒸気50を加熱双方の噴射出力を増大し、燃焼器1Yの複数燃焼ガス噴射ノズル6Yを過熱蒸気溜95c外周に具備して、1段噴射流の中に夫々の燃料噴射ノズル6Xより燃料噴射2段燃焼器複数燃焼にし、過熱蒸気50を外周より加熱して噴射出力と燃焼ガス吸引出力を増大して、環状の燃焼ガス噴射ノズル6Yの噴射流の内部に複数の3段燃焼器燃料噴射燃焼燃焼ガス噴射を可能にし、環状の燃焼ガス噴射ノズル6Y噴射流内部に複数の燃焼ガス噴射ノズル6Yを具備して、夫々の燃料噴射ノズル6Xより燃料噴射3段燃焼器複数燃焼にし、既存ジェット機の10〜100倍圧力10倍質量の安価な噴射出力狙いにします。 The combined engine injection unit 78S in FIG. 5 supplies the superheated steam 50 divided and stored by opening the superheated steam control valve 25 to the uppermost stream of the superheated steam reservoir 95c on the outer periphery of the combustor 1Y. In the process of producing superheated steam 50, fuel is injected and burned into compressed air 28a, compressed multiple times by the compressed heat recovery unit 2C and recovered multiple times by fuel injection and combustion, and infinitely high pressure combustion gas 49 oxidant and superheated steam 50 propellant is increased without limit, the combustion gas control valve 24 is opened at the time of ascending space, and the combustion gas 49 is supplied to the uppermost stream of the combustion gas reservoir 95a combustor 1Y by supplying the combustion gas 49 around 200 degrees to the fuel control. Fuel 1b is injected from the fuel injection nozzle 6X by the valve 25b open fuel injection pump 1D, and the superheated steam 50 on the outer periphery of the ignition combustion can be increased in the uppermost stream of the combustor 1Y. 95c, around 400 degrees, 24 to 400 MPa, superheated steam 50 is heated to increase both injection outputs, and a plurality of combustion gas injection nozzles 6Y of the combustor 1Y are provided on the outer periphery of the superheated steam reservoir 95c, each in a single-stage injection flow. The fuel injection nozzle 6X is used for multiple combustion of the fuel injection two-stage combustor, the superheated steam 50 is heated from the outer periphery, and the injection output and the combustion gas suction output are increased. A plurality of three-stage combustor fuel injection combustion combustion gas injection is possible, and a plurality of combustion gas injection nozzles 6Y are provided inside the annular combustion gas injection nozzle 6Y injection flow, and fuel injection three-stage from each fuel injection nozzle 6X Use multiple combustors and aim for inexpensive jet output with 10 to 100 times the pressure and 10 times the mass of existing jets.

液体酸素の圧入が必要な場合は圧縮熱回収器2C燃焼の過程で圧入して、理論空燃比に近付けた超高速噴射にし、過熱蒸気50の低温噴射と燃焼ガス49の高温噴射を合体して、夫々の長所を利用最良の組み合わせにした理論最良の合体機関噴射部78Sとし、既存のスクラムジェット+ロケット+蒸気タービンの長所とも合体構成して、大気中を飛行時には圧縮熱回収器2Cの燃焼が不要で、上記燃焼ガス制御弁24開放が圧縮空気制御弁24A開放となり、太陽光加熱の空気28aを圧縮し、800〜1200度にして圧縮熱回収器2Cで熱交換過熱蒸気50の推進剤製造に専念して、主として過熱蒸気50による噴射推進とし、1段燃焼も2段燃焼も3段燃焼も僅少にする地球温暖化防止推進として、20度に近付く過熱蒸気50を500度等に加熱噴射推進出力を大幅に増大し、過熱蒸気容積の大部分を増大噴射速度を増大燃焼ガス49の吸引力を増大して、最も効率良く過熱蒸気50と燃焼ガス49を混合噴射する合体機関噴射部78Sを駆動し、既存のスクラムジェット+ロケット+蒸気タービンの長所のみ利用して、過熱蒸気50や燃焼ガス49や圧縮空気28aの酸化剤や推進剤を保存使用し、円筒回転部77Gを180度以上の回転にして垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や宇宙利用全盛にし、地球上何処でも日帰り旅行等を可能にします。 When injection of liquid oxygen is required, it is injected during the combustion process of the compression heat recovery unit 2C to achieve ultra-high speed injection close to the theoretical air-fuel ratio, and the low temperature injection of superheated steam 50 and the high temperature injection of combustion gas 49 are combined. Combining with the advantages of the existing scramjet + rocket + steam turbine, and combining the advantages of each of the advantages of the best combined use engine injection section 78S, combustion of the compressed heat recovery unit 2C when flying in the atmosphere The combustion gas control valve 24 is opened to the compressed air control valve 24A, the solar heating air 28a is compressed to 800 to 1200 degrees, and the propellant of the heat exchange superheated steam 50 in the compression heat recovery unit 2C. Focusing on manufacturing, mainly using superheated steam 50 as a propulsion propulsion system to prevent global warming by reducing one-stage combustion, two-stage combustion, and three-stage combustion, the superheated steam 50 approaching 20 degrees The heating injection propulsion output is greatly increased to 0 degrees, the majority of the superheated steam volume is increased, the injection speed is increased, the suction force of the combustion gas 49 is increased, and the superheated steam 50 and the combustion gas 49 are mixed and injected most efficiently. The combined engine injection unit 78S is driven, and only the advantages of the existing scramjet + rocket + steam turbine are used, and the oxidizer and propellant of the superheated steam 50, combustion gas 49 and compressed air 28a are stored and used, and the cylinder rotates. By rotating the part 77G more than 180 degrees, vertical ascent, vertical descent, and reverse injection are possible, making the airfield and space use prime everywhere, and making day trips anywhere on the earth.

0:真空、 1:発電機、 1A:水銀排気検査室、 1B:酸素量増大手段、 1C:アルコール冷熱、 1D:燃料噴射ポンプ、 1F:復水ポンプ、 1G:熱ポンプ、 1H:揚水ポンプ、 1J:揚水装置、 1Y:燃焼器、 1b:燃料、 1c:比重大物質、 1d:水銀、 1e:被覆鋼球(衝撃低減手段2Gで被覆) 1e:被覆水銀(球形のステンレス等耐久材や衝撃低減手段2Gで被覆) 1g:重力加速部、 1h:横軸、 2:太陽光加熱器(長レンズで太陽光を傾斜回転して追跡) 2a:水復水器、 2b:太陽熱増大吊橋(吊具左右を上下して長レンズ複数段で太陽光を傾斜回転して追跡) 2c:断熱材、 2d:長レンズ、 2e:水面、 2f:吊具左、 2g:吊具右、 2A:耐熱材、 2B:熱吸収材、 2C:圧縮熱回収器、 2D:出力増大手段、 2E:出力増大球(水銀・液体鉛・液体錫・液体ビスマス・液体カドミウム・液体インジウム・液体ガリウム・液体亜鉛・液体タリウム・液体金属・水・白金球・被覆白金球・金球・被覆金球・白金合金球・金合金球・鉛合金球・銀合金球・被覆白金合金球・被覆金合金球・被覆鉛球・被覆銀合金球・タングステン合金球・被覆タングステン合金球・タングステン鋼球・被覆タングステン鋼球・タンタル合金球・被覆タンタル合金球・モリブデン鋼球・被覆モリブデン鋼球・モリブデン鋳鉄球・被覆モリブデン鋳鉄球・銀球・被覆銀球) 2F:増大球上昇装置、 2G:衝撃低減手段(小径球・潤滑油類・不燃液体類・ゴム類・プラスチック類等の被覆) 2H:冷熱復水器、 2J:液体金属熱交換器、 2K:潤滑性材料、 2X:空気熱交換器、 2Y:水熱交換器、 2Z:水銀熱交換器、 3:摩擦損失低減手段(撥水作用や加熱高温手段や被覆等最適利用公知技術で摩擦損失を低減) 3A:撥水作用(水との摩擦損失低減手段) 3B:加熱高温手段(電気抵抗や電磁加熱等既存技術で高温にする) 3C:冷熱回収手段、 3G:撥水作用(水銀との摩擦損失低減手段) 4A:タービン翼断面(既存断面) 4B:タービン翼断面(出力面湾曲少断面) 4C:タービン翼断面(出力面直線断面) 4D:タービン翼断面(出力反対面直線断面) 4E:タービン翼断面(出力反対面湾曲少断面) 4F:タービン翼断面(既存の反対断面) 4X:タービン翼断面(4A〜4Fより選択断面) 5C:空気排気室、 6:ノズル、 6a:ノズル噴射部、 6b:ノズル噴射部、 6d:ノズル噴射部、 6z:水噴射ポンプ、 6A:過熱蒸気噴射ノズル、 6B:液体鉛噴射ポンプ、 6C:液体錫噴射ポンプ、 6D:液体ビスマス噴射ポンプ、 6E:液体亜鉛噴射ポンプ、 6F:圧縮空気噴射ノズル、 6H:液体カドミウム噴射ポンプ、 6I:液体インジウム噴射ポンプ、 6J:液体ガリウム噴射ポンプ、 6K:液体タリウム噴射ポンプ、 6L:液体金属噴射ポンプ、 6X:燃料噴射ノズル、 6Y:燃焼ガス噴射ノズル、 6Z:水銀噴射ポンプ、 7:燃料噴射弁、 7A:プロペラ、 7B:回転翼、 7C:スクリュー、 7E:回転腕翼、 8a:全動翼弾み車ガスタービン(全動翼ガスタービン又は全動翼質量タービン)、 8b:全動翼弾み車水タービン(全動翼水タービン又は全動翼熱量タービン)、 8c:タービン翼、 8d:側板、 8e:円筒胴、 8E:全動翼弾み車水銀タービン(全動翼水銀タービン又は全動翼熱量タービン)8F:全動翼弾み車重力タービン、8G:竪型全動翼重力太陽熱タービン(竪型全動翼熱量タービン+竪型全動翼質量タービン)、 8K:液体金属重力対向タービン(対向タービン対向熱量タービン対向質量タービン)、8K:対向直列全動翼弾み車タービン(対向直列全動翼弾み車水銀タービン対向直列全動翼弾み車水タービン対向直列全動翼弾み車ガスタービン対向直列全動翼弾み車重力タービン)、 8L:直列全動翼弾み車タービン(直列全動翼弾み車水銀タービン直列全動翼弾み車水タービン直列全動翼弾み車ガスタービン直列全動翼弾み車重力タービン)、 10:船体、 10a:拡径圧縮室、10b:操縦室、 10c:制御室、 10d:客室、 10e:貨物室、 11A:隔壁、 11B:水室 11C:空気室、 11D:真空室、 16:クランク軸、16A:水平軸、 21:拡径ピストン、24:燃焼ガス制御弁、 24A:圧縮空気制御弁、 25:過熱蒸気制御弁、 25B:高温水制御弁、 25a:吸気弁、 25b:燃料制御弁、 28a:空気、 28a:内部空気、 28a:空気管空気、 28b:圧縮空気熱量、 28A:吸入空気路、 28B:空気路入口、 37a:着磁摩擦車、 37b:内着磁摩擦車、 38a:飛行胴、 38b:飛行翼、 38c:飛行尾翼、 38d:垂直翼、 38e:翼前縁心、 38g:水上翼、 38A:重力飛行機、 38B:空気噴射船舶、 38C:水噴射船舶、 39A:太陽熱重力飛行機、 39A:液体金属重力太陽熱宇宙往還機、 39B:太陽熱重力回転飛行機、 39B:液体金属重力太陽熱飛行機、 39C:太陽熱重力ヘリコプター、 39C:液体金属重力太陽熱飛行船舶、 39D:スクリュー船舶、 39D:液体金属重力太陽熱船舶、 39F:宇宙往還機、 39G:宇宙往還飛行船舶、 40A:方向舵、 46:磁石部、 49:燃焼ガス、 49B:煙突燃焼ガス熱量、 49C:工場使用熱量、 50:過熱蒸気、 51:空気抽出器、 52a:水、 52b:水(太陽光で温度が変る水) 52b:高温水、 52d:温熱、 52d:水温熱、 52d:過熱蒸気温熱、 52e:冷熱、 52e:水冷熱、 52e:圧縮空気冷熱、 52e:アルコール冷熱、 52e:氷冷熱、 55:歯車式同期装置(磁気摩擦同期装置を含む) 55B:磁気摩擦変速装置(歯車式及び送水ポンプ兼用を含む) 55Y:歯車式変速装置(既存変速機から選択) 60A:内側軸装置、 60B:外側軸装置、 60C:内側動翼群、 60D:外側動翼群、 77B:筒形外箱、 77D:ウォータージェット外箱、 77F:噴射部外箱、 77G:円筒回転部、 77a:タービン外箱、 78K:合体機関噴射部、 78S:合体機関噴射部(スクラムジェット+蒸気タービン他) 79K:合体機関噴射部、 79M:ウォータージェット、 80:軸受、 80a:推力軸受、 80A:継手、 80B:締付具、 81:支軸、 81a:支点、 84:二重反転磁気摩擦動力伝達装置(歯車式及び送水ポンプ兼用を含む) 84Y:二重反転歯車装置(既存技術) 94:固定外箱、 94A:外箱垂直部、 95:高温水溜、 95a:燃焼ガス溜、 95b:圧縮空気溜、 95c:過熱蒸気溜、 95A:吸水路、 95B:燃料溜、 96A:送水路、 97:逆止弁、103:冷熱回収器、   0: Vacuum, 1: Generator, 1A: Mercury exhaust inspection room, 1B: Oxygen amount increasing means, 1C: Alcohol cooling, 1D: Fuel injection pump, 1F: Condensate pump, 1G: Heat pump, 1H: Pumping pump, 1J: Pumping device, 1Y: Combustor, 1b: Fuel, 1c: Specific critical material, 1d: Mercury, 1e: Coated steel ball (covered with impact reducing means 2G) 1e: Coated mercury (durable material such as spherical stainless steel and impact 1g: Gravity acceleration part, 1h: Horizontal axis, 2: Solar heater (tracking by tilting and rotating sunlight with long lens) 2a: Water condenser, 2b: Solar thermal increase suspension bridge (suspended) 2c: heat insulating material, 2d: long lens, 2e: water surface, 2f: hanger left, 2g: hanger right, 2A: heat resistant material 2B: heat absorbing material, 2C: Reduced heat recovery unit, 2D: output increasing means, 2E: output increasing sphere (mercury, liquid lead, liquid tin, liquid bismuth, liquid cadmium, liquid indium, liquid gallium, liquid zinc, liquid thallium, liquid metal, water, platinum sphere・ Coated platinum balls, gold balls, coated gold balls, platinum alloy balls, gold alloy balls, lead alloy balls, silver alloy balls, coated platinum alloy balls, coated gold alloy balls, coated lead balls, coated silver alloy balls, tungsten alloy balls, Coated tungsten alloy balls, tungsten steel balls, coated tungsten steel balls, tantalum alloy balls, coated tantalum alloy balls, molybdenum steel balls, coated molybdenum steel balls, molybdenum cast iron balls, coated molybdenum cast iron balls, silver balls, coated silver balls) 2F: Expanding sphere raising device, 2G: Impact reduction means (Coating with small-diameter spheres, lubricating oils, incombustible liquids, rubbers, plastics, etc.) 2H: Cooling / cooling condenser, 2J: Liquid metal heat exchanger , 2K: Lubricating material, 2X: Air heat exchanger, 2Y: Water heat exchanger, 2Z: Mercury heat exchanger, 3: Friction loss reducing means (water repellent action, heating high temperature means, coating, etc. 3A: Water repellent action (means for reducing friction loss with water) 3B: High temperature heating means (high temperature with existing technology such as electric resistance and electromagnetic heating) 3C: Cold recovery means 3G: Water repellent action ( 4A: Turbine blade cross section (existing cross section) 4B: Turbine blade cross section (output surface curved small cross section) 4C: Turbine blade cross section (output surface straight cross section) 4D: Turbine blade cross section (output opposite surface straight line) Cross section) 4E: Turbine blade cross section (curved cross section on the opposite surface of the output) 4F: Turbine blade cross section (existing opposite cross section) 4X: Turbine blade cross section (cross section selected from 4A to 4F) 5C: Air exhaust chamber 6: Nozzle 6 : Nozzle injection unit, 6b: nozzle injection unit, 6d: nozzle injection unit, 6z: water injection pump, 6A: superheated steam injection nozzle, 6B: liquid lead injection pump, 6C: liquid tin injection pump, 6D: liquid bismuth injection pump 6E: liquid zinc injection pump, 6F: compressed air injection nozzle, 6H: liquid cadmium injection pump, 6I: liquid indium injection pump, 6J: liquid gallium injection pump, 6K: liquid thallium injection pump, 6L: liquid metal injection pump, 6X: Fuel injection nozzle, 6Y: Combustion gas injection nozzle, 6Z: Mercury injection pump, 7: Fuel injection valve, 7A: Propeller, 7B: Rotary blade, 7C: Screw, 7E: Rotary arm blade, 8a: Full bucket blade wheel Gas turbine (all blade gas turbine or all blade mass turbine), 8b: all blade impeller water turbine 8c: Turbine blades, 8d: Side plate, 8e: Cylindrical cylinder, 8E: Full blade flywheel mercury turbine (full blade mercury turbine or full blade heat quantity turbine) 8F: all-blade flywheel gravity turbine, 8G: vertical all blade gravity solar thermal turbine (vertical total blade calorific value turbine + vertical all blade mass turbine), 8K: liquid metal gravity opposed turbine (opposed turbine opposed calorific value turbine) Opposed Mass Turbine), 8K: Opposed Series Full Rotor Pusher Turbine (Opposed Series Full Rotor Pusher Mercury Turbine Opposed Series Full Rotor Pusher Water Turbine Opposed Series Full Rotor Pusher Car Gas Turbine Opposed Series Full Rotor Pusher Gravity Turbine), 8L : Series all blade impeller turbine (series all blade impeller mercury turbine series all blade impeller water turbine series all blade impeller gas turbine series all blade impeller 10b: cockpit, 10c: control room, 10d: cabin, 10e: cargo compartment, 11A: bulkhead, 11B: water chamber, 11C: air chamber, 11D: vacuum 16: Crankshaft, 16A: Horizontal shaft, 21: Expanded piston, 24: Combustion gas control valve, 24A: Compressed air control valve, 25: Superheated steam control valve, 25B: Hot water control valve, 25a: Intake valve 25b: Fuel control valve, 28a: Air, 28a: Internal air, 28a: Air tube air, 28b: Compressed air calorie, 28A: Intake air passage, 28B: Air passage inlet, 37a: Magnetized friction wheel, 37b: Inside Magnetized friction wheel, 38a: flight trunk, 38b: flight wing, 38c: flight tail, 38d: vertical wing, 38e: wing leading edge, 38g: surface wing, 38A: gravity airplane, 8B: Air-injected ship, 38C: Water-injected ship, 39A: Solar thermal gravity plane, 39A: Liquid metal gravity solar thermal spacecraft, 39B: Solar thermal gravity rotating plane, 39B: Liquid metal gravity solar thermal plane, 39C: Solar thermal gravity helicopter, 39C : Liquid metal gravity solar thermal ship, 39D: Screw ship, 39D: Liquid metal gravity solar ship, 39F: Space return aircraft, 39G: Space return flight ship, 40A: Rudder, 46: Magnet part, 49: Combustion gas, 49B: Chimney combustion gas calorific value, 49C: Factory calorific value, 50: Superheated steam, 51: Air extractor, 52a: Water, 52b: Water (water whose temperature changes with sunlight) 52b: Hot water, 52d: Thermal energy, 52d: Water Warm temperature, 52d: Superheated steam temperature, 52e: Cold heat, 52e: Water-cooled heat, 52e: Compressed air cooling 52e: alcohol cooling / heating 52e: ice cooling / heating 55: gear type synchronous device (including magnetic friction synchronous device) 55B: magnetic friction transmission device (including gear type and water pump combined use) 55Y: gear type transmission (existing speed change) 60A: Inner shaft device, 60B: Outer shaft device, 60C: Inner blade group, 60D: Outer blade group, 77B: Cylindrical outer box, 77D: Water jet outer box, 77F: Injection unit outer box 77G: Cylindrical rotating part, 77a: Turbine outer box, 78K: Combined engine injection part, 78S: Combined engine injection part (scramjet + steam turbine, etc.) 79K: Combined engine injection part, 79M: Water jet, 80: Bearing, 80a: thrust bearing, 80A: joint, 80B: clamp, 81: support shaft, 81a: fulcrum, 84: counter rotating magnetic friction power transmission (Including gear type and water pump) 84Y: Counter-rotating gear device (existing technology) 94: fixed outer box, 94A: vertical part of outer box, 95: hot water reservoir, 95a: combustion gas reservoir, 95b: compressed air Reservoir, 95c: Superheated steam reservoir, 95A: Water intake channel, 95B: Fuel reservoir, 96A: Water supply channel, 97: Check valve, 103: Cold heat recovery device,

Claims (5000)

タービン翼断面(4A)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 2 to 26 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + fuel cost little CO2 exhaust little coalescence engine injection part (78S) Propulsion output increase + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity Various energy storage cycle coalescing engines with a group of bolts of the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + fuel cost little CO2 exhaust little coalescence engine injection part (78S) injection propulsion output Increase + heat retention increase ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 6 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + fuel cost little CO2 exhaust little coalescence engine injection part (78S) injection propulsion output Increase + heat retention increase ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + fuel cost is small CO2 exhaust small coalescence engine injection part (78S) injection propulsion output Increase + heat retention increase ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + low fuel cost CO2 exhaust slight coalescence engine injection part (78S) injection propulsion output Increase + heat retention increase ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used. + Compressed air production heat production with compressed air calorie, mass, and liquid metal gravity Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with each blade having the same diameter and shape. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production + Combined engine of various energy storage cycle with turbine rotor blade group of same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending storage of metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production heat + Various energy storage cycles with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending storage of metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production heat + Various energy storage cycles with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending storage of metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production heat + Various energy storage cycles with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. that is divided and stored in heat and mass of compressed air. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. that is divided and stored in heat and mass of compressed air. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Various energy storage cycle coalescing engines that use metal ascending storage and heat-acceleration turbine that accelerates with pressure etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is driven to accelerate the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used for ascending and storing the liquid metal + Compressed air production heat production with compressed air calorie and mass and liquid metal gravity + Turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine Various energy conservation cycle coalescence engine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine is driven to accelerate the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used for ascending and storing the liquid metal + Compressed air production heat production with compressed air calorie and mass and liquid metal gravity + Turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine Various energy conservation cycle coalescence engine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine is driven to accelerate the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to store and store liquid metal + Compressed air production and production with compressed air calorie, mass, and liquid metal gravity + Assembly bolt assembly with turbine blades of the same diameter and shape of each paragraph Combined engine with various energy storage cycles as a turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Accelerating with increased output sphere (2E) as small diameter + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and the same shape for each stage Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Accelerating with increased output sphere (2E) as small diameter + Compressed air production and production with compressed air calorie, mass, and liquid metal gravity Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Accelerating with increased output sphere (2E) as small diameter + Compressed air production and production with compressed air calorie, mass, and liquid metal gravity Combined engine with various energy storage cycles as an assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Accelerating with increased output sphere (2E) as small diameter + Compressed air production and production with compressed air calorie, mass, and liquid metal gravity Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Accelerates by increasing the power increase sphere (2E) with a small diameter + Compressed air heat quantity, mass and liquid metal gravity to produce compressed air production heat + Turbine blade group for each paragraph with the same diameter and almost the same shape Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle Accelerated driving of liquid metal downward with alternating heat retaining turbines + Accelerated turbine driving with a small diameter increase in output sphere (2E) + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + Turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat-retaining turbines + Drives accelerated turbine with small output increase sphere (2E) diameter + Manufactures compressed air production heat with compressed air calorie, mass and liquid metal gravity + Stages of turbine blades Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angle and rotating direction Accelerated driving of liquid metal downward with alternating heat retaining turbines + Accelerated turbine driving with a small diameter increase in output sphere (2E) + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + Turbine blade group Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerated driving of liquid metal downward with alternating heat retaining turbines + Accelerated turbine driving with a small diameter increase in output sphere (2E) + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + Turbine blade group Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerated driving of liquid metal downward with alternating heat retaining turbine + Accelerated turbine driving with small output increase sphere (2E) + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Turbine blades per paragraph Various energy storage cycle coalescing engines with a group of bolts of the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air calorie, mass and liquid metal gravity to produce heat production + Compressed air production heat production + Turbine blade group for each stage is approximately the same shape for each stage, and a variety of energy storage cycles combined into a fitting bolt assembly turbine organ. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group of same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + Compressed air production heat production with heat quantity, mass and liquid metal gravity of the compressed air Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is driven downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is driven downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + output increase sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with a right angle square outer casing at right angles Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is driven downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + output increase sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is driven downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + output increase sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19-times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) configuration and method for accelerating power increase sphere (2E) + heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + output increase sphere (2E) configuration and method to accelerate + heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar heat engine + Configuration and method for accelerating output increase sphere (2E) ++ Increase in heat retention increase sphere The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 23 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + power increase ball (2E) configuration and method to accelerate + heat retention increase ball rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production and heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group for each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) high-propulsion propulsion output liquid metal solar engine + output increase sphere (2E) configuration and method to accelerate + heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) ++ Increase in heat retention increase sphere The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) configuration and method for accelerating power increase sphere (2E) + heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) ++ Increase in heat retention increase sphere The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating power increase sphere (2E) ++ Heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production and heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group for each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production + Combined engine of various energy storage cycle with turbine rotor blade group of same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4b)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4b) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending storage. + Compressed air calorie, mass, and liquid metal gravity are used to produce compressed air. Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending storage. + Compressed air calorie, mass, and liquid metal gravity are used to produce compressed air. Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending storage. + Compressed air calorie, mass, and liquid metal gravity are used to produce compressed air. Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending storage. + Compressed air calorie, mass, and liquid metal gravity are used to produce compressed air. Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the outer corner of the square turbine to save and use liquid metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production heat Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is equipped with right angled square outer casing and driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Directional alternating turbine + + heat retention increasing ball lift device (2F) is installed at the corner of the square turbine outer box to use liquid metal ascending and stored + compressed air production heat production and mass production of liquid metal gravity + turbine Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is equipped with right angled square outer casing and driven to rotate Directional alternating turbine + + heat retention increasing ball lift device (2F) is installed at the corner of the square turbine outer box to use liquid metal ascending and stored + compressed air production heat production and mass production of liquid metal gravity + turbine Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Directional alternating turbine + + heat retention increasing ball lift device (2F) is installed at the corner of the square turbine outer box to use liquid metal ascending and stored + compressed air production heat production and mass production of liquid metal gravity + turbine Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Directional alternating turbine + + heat retention increasing ball lift device (2F) is installed at the corner of the square turbine outer box to use liquid metal ascending and stored + compressed air production heat production and mass production of liquid metal gravity + turbine Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Directional alternating turbine + + heat retention increasing ball lift device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + compressed air production heat production by mass and liquid gravity of compressed air + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is equipped with right angled square outer casing and driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravitational acceleration and turbine driven + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravitational acceleration and turbine driven + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravitational acceleration and turbine driven + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angle square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravitational acceleration and turbine driven + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) is doubled turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angle square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravitational acceleration and turbine driven + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) is doubled turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angle square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) driven with right angle to square turbine outer box Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) is doubled turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 6 times turbine multiple drive short time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + power increase ball (2E) configuration and method to accelerate + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate the structure and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage and a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage. Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time combined engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Configuration and method for accelerating the liquid metal solar engine + output increasing sphere (2E) to make the turbine blade cross section (4E) 14 times the turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage and a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production + Combined engine of various energy storage cycle with turbine rotor blade group of same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending storage of metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production heat + Various energy storage cycles with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Various energy storage cycle coalescing engines that use heat storage turbines that are accelerated and driven by pressure, etc. divided and stored in compressed air heat quantity and mass. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity. Various energy conservation cycle coalescence engine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to store and use liquid metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production + Assembly of turbine rotor blades for each stage with the same diameter and the same shape for each stage Various energy storage cycle coalescing engine as turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) driven with right angle to square turbine outer box Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with a right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angle square outer box right angle drive and rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) driven with right angle to square turbine outer box Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with a right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) driven with right angle to square turbine outer box Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy conservation cycle coalescing engines with moving blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group of same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) is driven with a right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy conservation cycle coalescing engines with moving blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + Compressed air production heat production with heat quantity, mass and liquid metal gravity of the compressed air Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar heat engine to make large injection propulsion output + power increase sphere (2E) accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box and driven to rotate Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy conservation cycle coalescing engines with moving blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + Compressed air production heat production with heat quantity, mass and liquid metal gravity of the compressed air Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air calorie, mass and liquid metal gravity to produce heat production + Compressed air production heat production + Turbine blade group for each stage is approximately the same shape for each stage, and a variety of energy storage cycles combined into a fitting bolt assembly turbine organ. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + Compressed air production heat production with heat quantity, mass and liquid metal gravity of the compressed air Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air calorie, mass and liquid metal gravity to produce heat production + Compressed air production heat production + Turbine blade group for each stage is approximately the same shape for each stage, and a variety of energy storage cycles combined into a fitting bolt assembly turbine organ. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group of same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + Compressed air production heat production with heat quantity, mass and liquid metal gravity of the compressed air Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven to rotate Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heat and cold production with intake air path length lens and sunlight + Insulation sphere raising device (2F) is installed at corner of outer corner of square turbine and liquid metal is raised and used for storage + Calorific value and mass of compressed air Compressed air production heat production with liquid metal gravity + various energy conservation cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing at right angle Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is equipped with right angled square turbine outer box driving and rotating Rotating turbine with direction alternated + Heating / cooling production with intake air path length lens and sunlight + Insulating sphere raising device (2F) installed at corner of outer box of square turbine to use liquid metal for rising storage and use + Compressed air heat quantity and mass Compressed air production heat production with liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and stored. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) installed at corner of outer corner of square turbine to use liquid metal for rising storage and use + Compressed air production heat production with compressed air heat quantity, mass and liquid metal gravity + per paragraph In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation temperature riser device (2F) is installed at corner corner of rectangular turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) equipped with right angle square outer casing at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce compressed air production heat production + Various energy storage cycle coalescence engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Compressed air heat quantity, mass, and liquid metal gravity to produce heat + Heat production of compressed air + Combined various energy storage cycles with turbine blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection propulsion force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescence engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by the combined engine injection part (78S) injection driving force + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Heat of compressed air, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Configuration and method for accelerating the liquid metal solar engine + output increasing sphere (2E) that makes the turbine blade cross section (4A) 16 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Configuration and method for accelerating the liquid metal solar engine + output increasing sphere (2E) to make the turbine blade cross section (4B) 17 times the turbine multiple drive short time combined engine injection part (78S) large injection propulsion output + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19-times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + output increase sphere (2E) acceleration and configuration + method of intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage and a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration structure and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Configuration and method for accelerating the liquid metal solar engine + output increasing sphere (2E) to make the turbine blade cross section (4B) 23 times the turbine multiple drive short time coalescence engine injection section (78S) large injection propulsion output + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + Combined engine of various energy storage cycles with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Configuration and method for accelerating the liquid metal solar engine + output increasing sphere (2E) to make the turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output + intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat with compressed air calorie, mass and liquid metal gravity Manufacture + various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage and a fitting bolt assembly turbine. タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) double turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 4 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending storage of metal + Compressed air calorie, mass, and liquid metal gravity to produce compressed air production + Various energy storage cycles with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine for each stage Combined organization. タービン翼断面(4C)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4C) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air production + Combined engine of various energy storage cycle with turbine rotor blade group of same diameter and same shape for each stage as fitting bolt assembly turbine. タービン翼断面(4D)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 8 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 11 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 15 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles, rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 16 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4B) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4C)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 18 times turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerate alternating rotation heat insulation liquid metal + Various flying vessels Combined engine injection part (78S) Drives the driving force for injection + Insulates and raises ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Compressed air with heat quantity, mass and liquid metal gravity Air production heat production + various energy storage cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4D)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and storing metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air heat + Combined engine of various energy storage cycles with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerated driving of liquid bismuth downward with alternating heat-retaining turbines + Combined engine injection unit (78S) for driving driving propulsive force for various flying vessels + Insulating sphere raising device (2F) provided at corners of square turbine outer box Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate direction An alternate heat-retaining turbine is used to accelerate the liquid zinc downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Various energy storage cycle coalescing engines with turbine rotor blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat retaining turbine is used to accelerate and drive the liquid thallium alloy downward. + A variety of flying ships are driven by a combined engine injection unit (78S). Ascending and using liquid metal + Compressed air production and heat production using compressed air calorie and mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades of the same diameter and shape of each turbine as fitting bolt assembly turbine . タービン翼断面(4B)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is a 23 times larger turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with a right angle square outer casing at right angle Alternately heat-insulating turbines that accelerate the liquid zinc alloy downward + Various flying ships are driven by the combined engine injection part (78S) injection driving force + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box Ascending and using liquid metal + Compressed air production and heat production using compressed air calorie and mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades of the same diameter and shape of each turbine as fitting bolt assembly turbine . タービン翼断面(4C)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerated driving of liquid gallium alloy downward with alternating heat retaining turbines + Combined engine injection unit (78S) for driving driving propulsive force of various flying vessels + Insulating bulge raising device (2F) provided at corners of square turbine outer box Ascending and using liquid metal + Compressed air production and heat production using compressed air calorie and mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades of the same diameter and shape of each turbine as fitting bolt assembly turbine . タービン翼断面(4D)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Use directional alternating turbines + Drive various types of flying ships with united engine injection unit (78S) injection driving force + Insulate and increase the use of liquid metal by installing a warming-increasing sphere lifting device (2F) at the corner of the square turbine outer box + Compressed air production heat production with compressed air calorific value, mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine blades set to the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4E)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine outer box drive Rotating turbines with alternating rotation direction + Combined engine injection unit (78S) to drive injection propulsion force + Insulation sphere lifting device (2F) is installed at the corner of square turbine outer box + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4F)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) right angle square turbine outer box drive Rotating turbines with alternating rotation direction + Combined engine injection unit (78S) to drive injection propulsion force + Insulation sphere lifting device (2F) is installed at the corner of square turbine outer box + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4A)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) 2 to 26 times turbine multiple drive short-time coalesced engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square outer casing drive Rotating turbines with alternating rotation direction + Combined engine injection unit (78S) to drive injection propulsion force + Insulation sphere lifting device (2F) is installed at the corner of square turbine outer box + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4B)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with large injection propulsion output Rotation direction alternate heat insulation turbine, liquid metal is accelerated and driven downward + various flying ships are driven by combined engine injection part (78S) injection driving force + heat insulation increase ball rising device (2F) at corner part of square turbine outer box Install and use liquid metal ascending and storage + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Heat energy of the turbine blade group for each stage is made into a fitting bolt assembly turbine with the same diameter and shape of each stage Conservation cycle coalescence organization. タービン翼断面(4C)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with large injection propulsion output Rotation direction alternate heat insulation turbine, liquid metal is accelerated and driven downward + various flying ships are driven by combined engine injection part (78S) injection driving force + heat insulation increase ball rising device (2F) at corner part of square turbine outer box Install and use liquid metal ascending and storage + Compressed air calorie, mass and liquid metal gravity to produce compressed air + Heat energy of the turbine blade group for each stage is made into a fitting bolt assembly turbine with the same diameter and shape of each stage Conservation cycle coalescence organization. タービン翼断面(4D)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 2 to 26 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with large injection propulsion output Rotation direction alternate heat insulation turbine, liquid metal is accelerated and driven downward + various flying ships are driven by combined engine injection part (78S) injection driving force + heat insulation increase ball rising device (2F) at corner part of square turbine outer box Various energy storage cycle coalescing engines that use a heated metal turbine that accelerates with the use of liquid metal that is stored in an ascending manner and pressure that is divided and stored in compressed air heat and mass. タービン翼断面(4E)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with large injection propulsion output Rotation direction alternate heat insulation turbine, liquid metal is accelerated and driven downward + various flying ships are driven by combined engine injection part (78S) injection driving force + heat insulation increase ball rising device (2F) at corner part of square turbine outer box Various energy storage cycle coalescing engines that use a heated metal turbine that accelerates with the use of liquid metal that is stored in an ascending manner and pressure that is divided and stored in compressed air heat and mass. タービン翼断面(4F)を2〜26倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) 2 to 26 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with large injection propulsion output Rotation direction alternate heat insulation turbine, liquid metal is accelerated and driven downward + various flying ships are driven by combined engine injection part (78S) injection driving force + heat insulation increase ball rising device (2F) at corner part of square turbine outer box Various energy storage cycle coalescing engines that use a heated metal turbine that accelerates with the use of liquid metal that is stored in an ascending manner and pressure that is divided and stored in compressed air heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rising by installing a heat-retaining and increasing sphere raising device (2F) at the corner of the square turbine outer casing + Compressed air calorie Combined with various energy storage cycle engines, which are thermal turbines that are accelerated and driven by the pressure that is divided and stored in mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量に分割保存した圧力等で加速駆動する保温タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rising by installing a heat-retaining and increasing sphere raising device (2F) at the corner of the square turbine outer casing + Compressed air calorie Combined with various energy storage cycle engines, which are thermal turbines that are accelerated and driven by the pressure that is divided and stored in mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed air heat quantity, mass, and liquid metal gravity. Compressed air production heat production. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed air heat quantity, mass, and liquid metal gravity. Compressed air production heat production. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed air heat quantity, mass, and liquid metal gravity. Compressed air production heat production. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed air heat quantity, mass, and liquid metal gravity. Compressed air production heat production. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation and use + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines with turbine blades of each stage having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and stored. + Compressed air production heat production with the compressed air calorific value, mass and liquid metal gravity + Turbine blade group has the same diameter per paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine that has a substantially identical shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + Various energy conservation cycle coalescence engine with turbine rotor blade group having the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square square turbine outer box to make rotation direction alternate heat insulation turbine and liquid metal downward + Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Calorie heat quantity and mass Compressed air production heat production with liquid metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescence engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternately heat retaining turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + Various energy storage cycle coalescence engine with turbine rotor blade group of same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+過熱蒸気速度や燃焼ガス速度で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Accelerates with superheated steam speed and combustion gas speed + Paragraph of turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+過熱蒸気速度や燃焼ガス速度で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Accelerates with superheated steam speed and combustion gas speed + Paragraph of turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+過熱蒸気速度や燃焼ガス速度で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Accelerates with superheated steam speed and combustion gas speed + Paragraph of turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) provided at right angles to the rectangular turbine outer box to make the rotating direction alternate heat-retaining turbine, the liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines in which turbine blade groups are set to be approximately the same shape and diameter for each paragraph, and a fitting bolt assembly turbine is used. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Compressed air production and heat production with compressed air calorie, mass and liquid metal gravity + Turbine blade group for each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+過熱蒸気速度や燃焼ガス速度で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Accelerates with superheated steam speed and combustion gas speed + Paragraph of turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとする各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines in which the blade group of each is made into a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines in which turbine blade groups are set to be approximately the same shape and diameter for each paragraph, and a fitting bolt assembly turbine is used. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+過熱蒸気速度や燃焼ガス速度で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Accelerates with superheated steam speed and combustion gas speed + Paragraph of turbine blade group Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the outer corner of the square turbine and uses the liquid metal ascending and storing + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + turbine Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternately heat retaining turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid Compressed air production heat production by metal gravity + various energy storage cycle coalescing engines with turbine blades having the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is lifted and used for storage + Compressed air production heat production with compressed air calorie, mass and liquid metal gravity + Various energy storage cycle coalescing engines in which turbine blade groups are set to be approximately the same shape and diameter for each paragraph, and a fitting bolt assembly turbine is used. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Compressed air production and production with compressed air calorie, mass and liquid metal gravity + Turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Calorie heat quantity, mass and liquid metal Compressed air production heat production by gravity + various energy storage cycle coalescing engines with turbine blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+圧縮空気熱量と質量と液体金属重力で圧縮空気製造熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball lifting device (2F) at the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Compressed air production heat production with mass and liquid metal gravity + various energy storage cycle coalescing engine with turbine rotor blade group with same diameter and same shape for each paragraph as fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball riser (2F) is installed at the corner of the square turbine outer box to store and use liquid metal. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine for large injection propulsion output + Liquid metal accelerated alternating rotation heat insulation turbine driven + Various airships combined engine injection unit (78S) injection propulsion force Drive + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. + Inlet air path length lens and solar heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy conservation cycle coalescing engines that use a long-length lens and sunlight for heating and cooling production + a turbine blade group with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy conservation cycle coalescing engines that use a long-length lens and sunlight for heating and cooling production + a turbine blade group with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy conservation cycle coalescing engines that use a long-length lens and sunlight for heating and cooling production + a turbine blade group with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection unit (78S) injection driving force + Insulating and increasing ball raising device (2F) at the corner of the outer corner of the square turbine to use the liquid metal for rising storage and use + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine for large injection propulsion output + Liquid metal accelerated alternating rotation heat insulation turbine driven + Various airships combined engine injection unit (78S) injection propulsion force Drive + heat retention increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection unit (78S) injection driving force + Insulating and increasing ball raising device (2F) at the corner of the outer corner of the square turbine to use the liquid metal for rising storage and use + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward + Driving various flying vessels with united engine injection unit (78S) injection driving force + Insulating and increasing ball raising device (2F) at the corner of the outer corner of the square turbine to use the liquid metal for rising storage and use + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward + Driving various flying vessels with united engine injection unit (78S) injection driving force + Insulating and increasing ball raising device (2F) at the corner of the outer corner of the square turbine to use the liquid metal for rising storage and use + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and sunlight for heating / cooling production + Heat retention increasing sphere raising device (2F) Increase head drop + Thermal insulation increasing sphere raising device (2F) at corner corner of rectangular turbine Uses ascending storage + Intake air path length lens and solar heating / cooling manufacturing + Uses turbine blades of each turbine with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and sunlight for heating / cooling production + Heat retention increasing sphere raising device (2F) Increase head drop + Thermal insulation increasing sphere raising device (2F) at corner corner of rectangular turbine Uses ascending storage + Intake air path length lens and solar heating / cooling manufacturing + Uses turbine blades of each turbine with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and sunlight for heating / cooling production + Heat retention increasing sphere raising device (2F) Increase head drop + Thermal insulation increasing sphere raising device (2F) at corner corner of rectangular turbine Uses ascending storage + Intake air path length lens and solar heating / cooling manufacturing + Uses turbine blades of each turbine with the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Increase head drop with warming increase sphere lifting device (2F) + Heat retention increase ball lifting device (2F) is installed at corner of outer corner of square turbine and liquid metal is lifted and used for storage + intake air path Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Increase head drop with warming increase sphere lifting device (2F) + Heat retention increase ball lifting device (2F) is installed at corner of outer corner of square turbine and liquid metal is lifted and used for storage + intake air path Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy conservation cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy conservation cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine for high injection propulsion output + Liquid metal accelerated alternating rotation heat insulation turbine drive + Various airplanes combined engine injection unit (78S) injection propulsion drive + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heat production are used. Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy conservation cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + The intake air path length lens and solar heat production are used. + The turbine blade group is set for each paragraph. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the square turbine outer casing + Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines with moving blade groups of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storing. + The intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight to produce hot and cold heat + a turbine assembly of turbine blades with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Manufactured and used + energy storage cycle coalescing engine with turbine rotor blades of the same diameter and same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by propulsion propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. In addition, various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Manufactured and used + energy storage cycle coalescing engine with turbine rotor blades of the same diameter and same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine that uses turbines with blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Manufactured and used + energy storage cycle coalescing engine with turbine rotor blades of the same diameter and same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine that uses turbines with blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of airplanes with united engine injection part (78S) injection driving force + Insulate and use liquid metal by assembling and keeping the liquid metal in the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Manufactured and used + energy storage cycle coalescing engine with turbine rotor blades of the same diameter and same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold heat in each + energy storage cycle coalescing engine with turbine rotor blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternate heat retaining turbine to accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing to save and use liquid metal Combined with various energy storage cycle engines, the turbine blades used in the hot and cold manufacturing are combined with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) provided at right angles to the rectangular turbine outer box to make the rotating direction alternate heat-retaining turbine, the liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and the sun are installed by using a warming and increasing sphere lifting device (2F) at the corner of the square turbine outer casing to ascend and store liquid metal Various energy storage cycle coalescence engine that uses heat and cold production with light + turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine that uses turbines with blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with the intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive in rotation direction alternate turbine + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascending and storing + Heating and cooling with intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for manufacture and a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive turbines with alternating rotation direction + Various airplanes Combined engine injection part (78S) Drives the driving force of injection + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal ascends and saves it Various energy storage cycle coalescing engines with a moving bolt group of turbines to be manufactured and made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+段落毎にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine blade group of each turbine with the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold / cooled heat + Combined engine with various energy storage cycles, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine for fully automatic processing. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) provided at right angles to the rectangular turbine outer box to make the rotating direction alternate heat-retaining turbine, the liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and the sun are installed by using a warming and increasing sphere lifting device (2F) at the corner of the square turbine outer casing to ascend and store liquid metal Various energy storage cycle coalescence engine that uses heat and cold production with light + turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades and fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser device (2F) at the corner of the square turbine outer casing and uses the liquid metal for rising storage and use + Intake air path length lens and sunlight Various energy storage cycle coalescing engines with a moving bolt group of turbines used for cold heat production, with the same diameter and shape of each turbine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescence engines that use a long lens and sunlight for heating and cooling production + a fully-automatically machined turbine blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight to produce hot and cold heat + a fully-automatic turbine blade group that has the same diameter and the same shape for each paragraph and is a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine for large injection propulsion output + Liquid metal accelerated alternating rotation heat insulation turbine driven + Various airships combined engine injection unit (78S) injection propulsion force Drive + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. + Inlet air path length lens and solar heat production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy storage cycle coalescence engines that use heat and cold production with road length lens and sunlight + full-automatic machining, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy storage cycle coalescence engines that use heat and cold production with road length lens and sunlight + full-automatic machining, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward + Accelerate driving + Drive various types of flying ships with united engine injection part (78S) injection driving force + Insulate air by using a warming and increasing ball raising device (2F) at the corner of the square turbine outer box Various energy storage cycle coalescence engines that use heat and cold production with road length lens and sunlight + full-automatic machining, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser (2F) at the corner of the square turbine outer casing and uses the liquid metal for storage and storage + Heated by the intake air path length lens and sunlight Various energy conservation cycle coalescence engines that are used for cold heat production + full-automatic machining, and the turbine blades are of the same diameter and shape of each stage and fitted with a bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser (2F) at the corner of the square turbine outer casing and uses the liquid metal for storage and storage + Heated by the intake air path length lens and sunlight Various energy conservation cycle coalescence engines that are used for cold heat production + full-automatic machining, and the turbine blades are of the same diameter and shape of each stage and fitted with a bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser (2F) at the corner of the square turbine outer casing and uses the liquid metal for storage and storage + Heated by the intake air path length lens and sunlight Various energy storage cycle coalescing engines that use a cold-heated manufacturing + fully automatic machining turbine blade group with the same diameter and shape of each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven to have a square turbine outer box at right angles to drive to rotate direction alternating turbine + Various flying ships + Combined engine injection unit (78S) Drives the driving force for injection + Insulates and increases the warming sphere riser (2F) at the corner of the square turbine outer casing and uses the liquid metal for storage and storage + Heated by the intake air path length lens and sunlight Various energy storage cycle coalescing engines that use a cold-heated manufacturing + fully automatic machining turbine blade group with the same diameter and shape of each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight to produce hot and cold heat + a fully-automatic turbine blade group that has the same diameter and the same shape for each paragraph and is a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight to produce hot and cold heat + a fully-automatic turbine blade group that has the same diameter and the same shape for each paragraph and is a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight to produce hot and cold heat + a fully-automatic turbine blade group that has the same diameter and the same shape for each paragraph and is a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Drives various flying vessels + Combined engine injection unit (78S) + Drives driving propulsion force + Insulates and uses liquid metal ascending and storing by installing a warming and increasing ball raising device (2F) at the corner of the rectangular turbine outer box Various energy conservation cycle coalescing engines that use a long lens and sunlight for heating and cooling production + turbine turbine blades with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Intake air path length lens and solar heating / cooling production + Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Intake air path length lens and solar heating / cooling production + Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Intake air path length lens and solar heating / cooling production + Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Conservation use + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and same shape for each stage as a fitting bolt assembly turbine . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Intake air path length lens and solar heating / cooling manufacturing use + Fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+液体金属を加速交互回転保温タービンを駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar heat engine that makes large injection propulsion output + Accelerate liquid metal alternately rotating heat insulation turbine + Intake air path length lens and solar heat production + heat insulation increase A ball lifter (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used for storage. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold / cooled heat + Combined engine with various energy storage cycles, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine for fully automatic processing. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerating with a small diameter + Intake air path length lens and using solar heat for heating and cooling + Various energy storage cycle coalescing engines with turbine blades having the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerates with small diameter + Uses intake air path length lens and heating / cooling production with sunlight + Various energy for turbine blade group with same diameter and almost same shape for each stage for fully automatic processing Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerates with small diameter + Uses intake air path length lens and heating / cooling production with sunlight + Various energy for turbine blade group with same diameter and almost same shape for each stage for fully automatic processing Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerates with small diameter + Uses intake air path length lens and heating / cooling production with sunlight + Various energy for turbine blade group with same diameter and almost same shape for each stage for fully automatic processing Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerates with small diameter + Uses intake air path length lens and heating / cooling production with sunlight + Various energy for turbine blade group with same diameter and almost same shape for each stage for fully automatic processing Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+出力増大球(2E)を小径として加速タービン駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) liquid metal solar thermal engine to make large injection propulsion output + horizontal axis (1h) is driven by a square turbine outer box at right angles to drive a rotating direction alternating turbine + output increasing sphere ( 2E) is driven by an accelerated turbine with a small diameter + used for intake air path length lens and solar heating / cooling production + combined turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Acceleration turbine drive with a small output sphere (2E) as a small diameter + Use of intake air path length lens and sunlight for heating / cooling / heating + Turbine blade group with the same diameter and the same shape for each stage Fitting bolt assembly turbine Various energy conservation cycle coalescing engines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Acceleration turbine drive with a small output sphere (2E) as a small diameter + Use of intake air path length lens and sunlight for heating / cooling / heating + Turbine blade group with the same diameter and the same shape for each stage Fitting bolt assembly turbine Various energy conservation cycle coalescing engines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Acceleration turbine driving with a small output increase sphere (2E) diameter + Intake air path length lens and solar heating / cooling manufacturing use + Turbine blade group with almost the same shape for each paragraph for fully automatic processing Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Accelerate turbine drive with a small output sphere (2E) diameter + Use intake air path length lens and solar heating / cooling manufacturing + Turbine blade group capable of fully automatic machining with almost the same shape for each paragraph Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a fully-automatically machined turbine blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use turbines and blades of a turbine that can be heated and cooled by using lenses and sunlight + a fully automatic machining turbine blade group with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+被覆白タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal to save and store + Use the intake air path length lens and solar heating and cooling production + Cover white Various energy conservation cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph and fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines that can be machined to make turbine blade groups with the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines, with a group of turbine blades that can be machined as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+液体カドミウムを加速転がり接触駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Inlet air path length lens and solar thermal heating / cooling production + Liquid cadmium Various energy conservation cycle coalescing engines, in which the rotor blades of a counter rotating turbine that is driven by accelerated rolling contact are made into a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines that can be machined to make turbine blade groups with the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにしタンタル合金球球を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, tantalum alloy ball down + Intake air path length lens and heating / cooling production with sunlight + Insulation air path length lens with a heat retention increasing sphere raising device (2F) installed at the corner of the outer corner of the square turbine to save and use liquid metal + Combined use of various energy storage cycle engines that use hot / cold manufacturing with sunlight + fully-automatic machining that allows the turbine blades to have the same diameter and the same shape for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+モリブデン鋼球を加速駆動の二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat and heat production are used. Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+液体錫を加速駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is lifted and used. + The intake air path length lens and solar light are used for heating and cooling. + The rotating blades of the counter-rotating turbine that accelerates the liquid tin. Various energy storage cycle coalescing engines with a group of bolts of the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+水銀を加速駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + The intake air path length lens and solar heat and heat production are used. + The rotating blade group of counter rotating turbine that accelerates mercury. Various energy storage cycle coalescing engines with a fitting bolt assembly turbine with the same diameter and shape as each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+被覆銀球を加速駆動の二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescence engine which uses the jointed silver sphere as a fitting bolt assembly turbine with the same diameter and the same shape for each stage of the rotating blades of the counter rotating turbine that is driven by acceleration. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+より液体カドミウム合金を加速駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Combined with various energy storage cycle engines, the rotor blades of the counter rotating turbine that accelerates and drives the liquid cadmium alloy with the same diameter and the same shape for each paragraph are used as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold / cooled heat + Combined engine with various energy storage cycles, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine for fully automatic processing. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a fully-automatically machined turbine blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use turbines and blades of a turbine that can be heated and cooled by using lenses and sunlight + a fully automatic machining turbine blade group with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+被覆タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines with the same group of blades of the same diameter and the same shape for each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines that can be machined to make turbine blade groups with the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+液体カドミウムを加速転がり接触駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Inlet air path length lens and solar thermal heating / cooling production + Liquid cadmium Various energy conservation cycle coalescing engines, in which the rotor blades of a counter rotating turbine that is driven by accelerated rolling contact are made into a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+液体インジウムを加速転がり接触駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage. Various energy conservation cycle coalescing engines, in which the rotor blades of a counter rotating turbine that is driven by accelerated rolling contact are made into a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+液体ガリウムを加速駆動する二重反転タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the outer corner of the square turbine to save and use liquid metal + Intake air path length lens and use for solar thermal heating and cooling + Liquid gallium Various energy conservation cycle coalescing engines in which the rotor blade group of the counter rotating turbine for accelerating the motor is made into a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ビスマスを下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine that makes large injection propulsion output + horizontal axis (1h) is equipped with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate liquid bismuth downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotating direction alternately heat retaining turbine, liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternately heat retaining turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Used in the production of hot / cold / cooled heat + Combined engine with various energy storage cycles, with turbine blades having the same diameter and shape of each paragraph as a fitting bolt assembly turbine for fully automatic processing. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal Various energy storage cycle coalescing engines with turbine blades of the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a turbine rotor blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use a lens and sunlight to produce hot and cold heat + a fully-automatically machined turbine blade group with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by assembling the warming-increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Intake air path length Various energy conservation cycle coalescence engines that use turbines and blades of a turbine that can be heated and cooled by using lenses and sunlight + a fully automatic machining turbine blade group with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines, with a group of turbine blades that can be machined as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines, with a group of turbine blades that can be machined as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsive force + Insulating and increasing ball lifting device (2F) is installed in the corner of the square turbine outer box to use and store liquid metal. Various energy storage cycle coalescing engines with moving blades as a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage. Various energy storage cycle coalescing engines that can be machined to make turbine blade groups with the same diameter and the same shape for each paragraph and a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternately warm turbine, accelerating the liquid zinc downward Driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sunlight by installing a heat retention increasing ball lift device (2F) at the corner of the square turbine outer casing to save and use liquid metal The energy storage cycle coalescing engine which uses the turbine rotor blade group with the same diameter and the same shape for each paragraph as the fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体タリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine, liquid thallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体亜鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) provided at right angles to the rectangular turbine outer box to make the rotating direction alternate heat-retaining turbine, the liquid zinc alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and the sun are installed by using a warming and increasing sphere lifting device (2F) at the corner of the square turbine outer casing to ascend and store liquid metal Various energy storage cycle coalescence engine that uses heat and cold production with light + turbine rotor blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体ガリウム合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat insulation turbine, liquid gallium alloy downward Accelerated driving + Intake air path length lens and solar heating / cooling production + Insulating air path length lens and sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades and fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed in the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and the solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Environmental energy storage cycle coalescing engine with a moving turbine group of turbines with the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar heat engine + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere increase The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method ++ heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere ++ The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Configuration and method for accelerating power increase sphere (2E) ++ Heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) configuration and method for accelerating power increase sphere +2 The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heat and cold manufacturing are used. Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere + The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 4 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output liquid metal solar engine + output increase sphere (2E) configuration and method for accelerating + heat retention increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere + The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending and storage. + Intake air path length lens and solar heat / cool manufacturing are used. Various energy storage cycle coalescing engine with fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere ++ The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heating / cooling production are used. Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate and increase heat retention increase sphere + The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + The intake air path length lens and solar heat and cold manufacturing are used. Various energy conservation cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles to rotate Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is used at the corner of the outer casing of the rectangular turbine, and the liquid metal is lifted and used. + The intake air path length lens and solar heat are used for heating and cooling. Combined engine with various energy storage cycles as a turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed in the corner of the outer casing of the square turbine, and the liquid metal is used for storage and preservation. + Inlet air path length lens and solar heating / cooling production is used. Various energy storage cycle coalescing engine as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Accelerates and drives liquid metal downward with alternating heat insulation turbines + Heat and cold production with intake air path length lens and sunlight + Heat drop increase device (2F) raises the head as much as possible + Heat increase ball increase device (2F) Is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used. + The intake air path length lens and solar heat are used for heating and cooling. + The turbine blades that can be fully automated are approximately the same diameter in each paragraph. Various energy storage cycle coalescing engine with fitting bolt assembly turbine as the same shape. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine casing at right angle A directional alternating turbine + + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle A directional alternating turbine + + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate A directional alternating turbine + + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Directional alternating turbine + + warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + use the intake air path length lens and sunlight to produce hot and cold heat + fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Directional alternating turbine + + warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use the liquid metal + use the intake air path length lens and sunlight to produce hot and cold heat + fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + output increasing sphere (2E) is accelerated downward by gravity acceleration turbine drive + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box and driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with right angle square turbine outer box driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box and driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated downward by gravity acceleration to drive turbine + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box and driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square outer casing drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) quadruple turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increasing sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration and configuration + method of intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades, with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short time combined engine injection part (78S) liquid metal solar engine + power increase sphere (2E) configuration and method to accelerate + injection air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades and fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase ball (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescence engines with turbine blades set to the same diameter and shape of each stage and fitted bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades, with the same diameter and shape of each paragraph, and a fitting bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Heating and cooling production with intake air path length lens and sunlight + Various energy storage cycle coalescing engines with fully-automatically machined turbine blades and fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S) injection driving force. + A heat-retaining and increasing ball lifting device (2F) is provided at the corner of the square turbine outer box. Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time combined engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) with right angled square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and storing metal + Uses intake air path length lens and sunlight for heating and cooling production + Saves various types of energy by using a turbine assembly with the same diameter and shape of each turbine as a fitting bolt assembly turbine for fully automatic processing Cycle coalescence engine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with same diameter and same shape for each stage Conservation cycle coalescence organization. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle An alternate heat-retaining turbine is used to accelerate the liquid metal downward. + A variety of flying ships are driven by the combined engine injection unit (78S). Uses ascending and preserving metal + Intake air path length lens and solar heating and cooling production + Combined engine of various energy storage cycles with turbine rotor blades of the same diameter and same shape for each paragraph and fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to use the liquid metal ascending and stored + Intake air path length lens and solar heating and cooling production + Various types of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine Energy conservation cycle coalescence engine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to use the liquid metal ascending and stored + Intake air path length lens and solar heating and cooling production + Various types of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine Energy conservation cycle coalescence engine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to use the liquid metal ascending and stored + Intake air path length lens and solar heating and cooling production + Various types of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine Energy conservation cycle coalescence engine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box to save and use the liquid metal + Use the intake air path length lens and solar heat for heating and cooling production + Fit the bolts of the turbine blade group with the same diameter and the same shape for each paragraph for fully automatic processing Various energy storage cycle coalescing engine as an assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine is used to accelerate and drive the liquid metal downward + Heat and cold production with intake air path length lens and sunlight + Increase head drop with heat increase ball lift device (2F) + Square heat turbine increase device (2F) with square heat turbine Installed at the corner of the outer box and used to store the liquid metal ascending + Combined with the intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining turbine blade group with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine with bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar heat engine to make large injection propulsion output + horizontal axis (1h) drive with right angled square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar heat engine to make large injection propulsion output + horizontal axis (1h) drive with right angled square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar heat engine to make large injection propulsion output + horizontal axis (1h) drive with right angled square turbine outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to the square turbine outer box Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar heat engine + horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward with gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and stored for use. Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and stored for use. Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) high injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with right angle square turbine casing right angle driven to rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) equipped with a rectangular turbine outer box at right angles and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angles Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Environmental energy storage cycle coalescence engine that uses turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic processing of turbine blades with the same diameter and shape of each stage as a fitting bolt assembly turbine for various energy storage cycles Combined organization. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Use of intake air path length lens and solar heating / cooling manufacturing + Fully automatic machining of turbine blades with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine Cycle coalescence engine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engine which uses turbines and blades of turbines with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades with the same diameter and the same shape for each stage to make fully automatic processing possible. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Various aircrafts are driven by a combined engine injection part (78S) injection driving force + A warming-increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and the liquid metal is raised and used for storage + Intake air path length lens and the sun Various energy storage cycle coalescence engines that use turbines and blades of the same diameter and the same shape for each stage as a group of turbine blades that can be used for light / hot / cool manufacturing and can be fully automated. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + horizontal axis (1h) is driven with right angled square turbine outer box at right angle Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Horizontal axis (1h) is driven with right angled square turbine outer box and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades of the turbine are used with the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is used. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times the turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angle square outer box drive and rotate Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy storage cycle engines, the turbine blades are of the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar engine + horizontal axis (1h) equipped with right angled square turbine outer box driven and rotated Inverted turbines + Intake air path length lens and solar heating / cooling manufacturing + Insulating air path length lens with a warming and increasing ball raising device (2F) installed at the corner of the square turbine outer box Combined with various energy conservation cycle engines, the turbine blades of the turbine that can be used for heating and cooling with sunlight and full-automatic machining can be made into a fitting bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) large injection propulsion output liquid metal solar thermal engine + horizontal axis (1h) with square turbine outer box at right angle and rotating direction Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Alternate heat insulation turbine + Insulation increase ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Intake air path length lens and sunlight to produce hot and cold heat + Turbine motion Various energy storage cycle coalescing engines with a blade group as a fitting bolt assembly turbine with a blade group of the same diameter and shape. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group is made into a fitting bolt assembly turbine with the same diameter and shape of each turbine as possible. タービン翼断面(4X)を2倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) double turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with square turbine outer box at right angle to rotate in the direction of rotation Alternate heat insulation turbine + Insulation sphere riser (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Inlet air path length lens and solar heating / cooling production + Fully automatic processing Various energy storage cycle coalescing engines, with the blades of the turbine capable of being used as a fitting bolt assembly turbine with the same diameter and shape of each paragraph. タービン翼断面(4X)を3倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 3 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を4倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 4 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を5倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 5 times turbine multiple drive short time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of solar energy for heating and cooling + Various energy conservation cycle coalescing engine with turbine blades of the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を6倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 6 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and solar heating / cooling production + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を7倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+吸入空気路長レンズと太陽光で温熱冷熱製造使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 7 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) to make large injection propulsion output right angle square turbine outer box at right angle Use alternating heat insulation turbine to accelerate liquid metal downward + Intake air path length lens and solar heating / cooling production + Insulation heat bulb increase device (2F) is installed at corner corner of square turbine and rises liquid metal + Intake air path length lens and use of sunlight for heating and cooling production + Various energy conservation cycle coalescing engine with fully automatic machining turbine blade group with the same diameter and the same shape for each paragraph as a fitting bolt assembly turbine. タービン翼断面(4X)を8倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 8 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Accelerates with combustion gas heat quantity and mass or compressed air calorie quantity and mass + Combines various energy storage cycle with turbine blades of the same diameter and same shape for each stage as a fitting bolt assembly turbine organ. タービン翼断面(4X)を9倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 9 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Accelerates with combustion gas heat quantity and mass or compressed air calorie quantity and mass + Combines various energy storage cycle with turbine blades of the same diameter and same shape for each stage as a fitting bolt assembly turbine organ. タービン翼断面(4X)を10倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 10 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle with square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Accelerates with combustion gas heat quantity and mass or compressed air calorie quantity and mass + Combines various energy storage cycle with turbine blades of the same diameter and same shape for each stage as a fitting bolt assembly turbine organ. タービン翼断面(4X)を11倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 11 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) with a square turbine outer box at right angles The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by a combined engine injection unit (78S). + Accelerate by pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy conservation cycle coalescence engine. タービン翼断面(4X)を12倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 12 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + horizontal axis (1h) at right angle to square turbine outer box at right angle The liquid metal is accelerated and driven downward by using alternate heat insulation turbines. + A variety of airplanes are driven by the combined engine injection part (78S). + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic machining with the same diameter and shape of each paragraph Various energy conservation cycle coalescence engine. タービン翼断面(4X)を13倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 13 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Drive various types of aircraft with united engine injection unit (78S) injection driving force + Insulate and increase ball riser device (2F) at corner of outer corner of square turbine to use and store liquid metal + Combustion gas heat quantity and mass or compression Various energy storage cycle coalescing engines that use a pressure divided and stored in the amount of air heat and mass, and make the turbine blades the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を14倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 14 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Drive various types of aircraft with united engine injection unit (78S) injection driving force + Insulate and increase ball riser device (2F) at corner of outer corner of square turbine to use and store liquid metal + Combustion gas heat quantity and mass or compression Various energy storage cycle coalescing engines that use a pressure divided and stored in the amount of air heat and mass, and make the turbine blades the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を15倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 15 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Drive various types of aircraft with united engine injection unit (78S) injection driving force + Insulate and increase ball riser device (2F) at corner of outer corner of square turbine to use and store liquid metal + Combustion gas heat quantity and mass or compression Various energy storage cycle coalescing engines that use a pressure divided and stored in the amount of air heat and mass, and make the turbine blades the same diameter and shape of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を16倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross-section (4X) 16 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine that makes large injection propulsion output + power increase sphere (2E) is accelerated turbine driven downward by gravitational acceleration + Drive various types of aircraft with united engine injection unit (78S) injection driving force + Insulate and increase ball riser device (2F) at corner of outer corner of square turbine to use and store liquid metal + Combustion gas heat quantity and mass or compression Various energy storage cycle coalescing engines in which turbine blades have the same diameter and the same shape for each stage and are fitted with bolt assembly turbines that can be accelerated and fully automated with the pressure stored separately in the amount of heat and mass of air. タービン翼断面(4X)を17倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 17 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) to accelerate turbine drive downward by gravitational acceleration + Drive various types of aircraft with united engine injection unit (78S) injection driving force + Insulate and increase ball riser device (2F) at corner of outer corner of square turbine to use and store liquid metal + Combustion gas heat quantity and mass or compression Various energy conservation cycle coalescing engines with turbine blades that can be accelerated and fully automatic processed by pressure divided and stored in air calorie and mass, and fitted with a bolt assembly turbine with the same diameter and shape of each stage. タービン翼断面(4X)を18倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 18 times turbine multiple drive short-time coalescence engine injection part (78S) Large metal propulsion output + liquid metal solar engine + output increase sphere (2E) configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン翼断面(4X)を19倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 19-times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase ball (2E) to accelerate large injection propulsion output + construction and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン翼断面(4X)を20倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 20 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン翼断面(4X)を21倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能にタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 21 times the turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with turbine rotor blades that have the same diameter and the same shape for each stage and are fitted with a bolt assembly turbine that can be accelerated and fully automatically machined at the same pressure. タービン翼断面(4X)を22倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 22 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined at the same pressure, with the same diameter and diameter of each stage as a fitting bolt assembly turbine. タービン翼断面(4X)を23倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 23 times turbine multiple drive short-time coalescence engine injection part (78S) Large injection propulsion output Liquid metal solar engine + Configuration and method for accelerating output increase sphere (2E) + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン翼断面(4X)を24倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 24 times turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar engine + power increase sphere (2E) configuration and method to accelerate + injection air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン翼断面(4X)を25倍のタービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4X) 25 times turbine multiple drive short-time coalescence engine injection section (78S) liquid metal solar engine + power increase sphere (2E) acceleration configuration and method + intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Divided and stored into combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with acceleration / acceleration + turbine blades and fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine is provided in one stage with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in two stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group of each stage with the same diameter and shape, and various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automatic processed with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in four stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine rotor blade group that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each paragraph, and with 5 stages of fitting bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine is provided in 8 stages, various energy storage cycle coalescence engine . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group of each stage with the same diameter and shape of each stage, and various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and approximately the same shape for each stage and fitting bolt assembly turbines provided in 10 stages, various energy storage cycle coalescence engine . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic machining possible Turbine blade group with the same diameter and shape of each stage, and a combination bolt assembly turbine in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and the same shape for each stage, and a combination bolt assembly turbine in two stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and the same shape for each stage, are provided with three stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automatic processed with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in four stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage are provided in five stages. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass are of the same diameter and shape of each stage, and are provided with 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, with the turbine blade group of turbines capable of acceleration + fully automatic processing, with the same diameter and the same shape for each stage, provided with 7 bolts of mating bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with 8 stages of bolt assembly turbines, with turbine blades that can be accelerated and fully automatic processed by pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine blade group that can be accelerated and fully-automatically processed with pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and with 9 bolted bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy conservation cycles with 10 stages of mating bolt assembly turbines, with turbine blades that can be accelerated and fully automatic processed with pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each paragraph Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine rotor blade group that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each stage, and a single bolted turbine assembly Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles in which the turbine blades that can be accelerated and fully automated by the pressure divided and stored in mass or compressed air calorie and mass are roughly the same shape for each stage, and the fitting bolt assembly turbine is provided in two stages. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage, and four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with five bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage, and 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air heat quantity and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with bolted turbine assembly in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines in which turbine blade groups are of the same shape for each stage and fitted with 10 bolts. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with a bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air heat quantity and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage, and four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with five bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Acceleration with pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each stage, 8 fitting bolt assembly turbines are provided Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining of turbine blades with the same diameter and shape of each stage in 9 stages of bolt assembly turbine Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic machining with 10 stages of mating bolt assembly turbines with the same diameter and shape of each stage Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and divided into combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are set to the same diameter and shape of each stage, and a variety of energy conservation is provided with one stage of fitting bolt assembly turbine Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are of the same shape for each stage and have the same diameter and shape, and two stages of fitting bolt assembly turbines for energy conservation Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing possible turbine Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing is possible Various energy storage cycle coalescing engines with turbine blade groups of the same diameter and shape of each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration + Fully automatic processing is possible with the pressure of combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines, in which the rotor blades of a simple turbine have substantially the same shape and the same diameter for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines with the same diameter and diameter of each paragraph, and with 6 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines, with the same diameter and diameter of each paragraph, and 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing possible turbine Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing is possible Various energy conservation cycle coalescing engines with turbine blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines arranged in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Acceleration + Fully automatic processing is possible with the pressure of combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine is provided in one stage with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in two stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group of each stage with the same diameter and shape, and various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automatic processed with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in four stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine rotor blade group that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each paragraph, and with 5 stages of fitting bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine is provided in 8 stages, various energy storage cycle coalescence engine . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group of each stage with the same diameter and shape of each stage, and various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and approximately the same shape for each stage and fitting bolt assembly turbines provided in 10 stages, various energy storage cycle coalescence engine . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic machining possible Turbine blade group with the same diameter and shape of each stage, and a combination bolt assembly turbine in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and the same shape for each stage, and a combination bolt assembly turbine in two stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and the same shape for each stage, are provided with three stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automatic processed with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in four stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage are provided in five stages. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, the turbine blades of the turbine that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass are of the same diameter and shape of each stage, and are provided with 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Combined with various energy storage cycles, with the turbine blade group of turbines capable of acceleration + fully automatic processing, with the same diameter and the same shape for each stage, provided with 7 bolts of mating bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with 8 stages of bolt assembly turbines, with turbine blades that can be accelerated and fully automatic processed by pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine blade group that can be accelerated and fully-automatically processed with pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and the same shape for each stage, and with 9 bolted bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy conservation cycles with 10 stages of mating bolt assembly turbines, with turbine blades that can be accelerated and fully automatic processed with pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each paragraph Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles with a turbine rotor blade group that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, with the same diameter and shape of each stage, and a single bolted turbine assembly Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Various energy storage cycles in which the turbine blades that can be accelerated and fully automated by the pressure divided and stored in mass or compressed air calorie and mass are roughly the same shape for each stage, and the fitting bolt assembly turbine is provided in two stages. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage, and four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with five bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage, and 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air heat quantity and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with bolted turbine assembly in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines in which turbine blade groups are of the same shape for each stage and fitted with 10 bolts. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with a bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air heat quantity and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage, and four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure divided and stored in mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups having the same diameter and shape of each stage and fitted with five bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage, and provided with six bolted assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored into mass or compressed air calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades having the same diameter and shape of each stage and fitted with a bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Acceleration with pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining possible Turbine blade group with the same diameter and the same shape for each stage, 8 fitting bolt assembly turbines are provided Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining of turbine blades with the same diameter and shape of each stage in 9 stages of bolt assembly turbine Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic machining with 10 stages of mating bolt assembly turbines with the same diameter and shape of each stage Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and divided into combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are set to the same diameter and shape of each stage, and a variety of energy conservation is provided with one stage of fitting bolt assembly turbine Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are of the same shape for each stage and have the same diameter and shape, and two stages of fitting bolt assembly turbines for energy conservation Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines with turbine blades capable of accelerating + fully automatic machining and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine blades of each turbine are of the same shape and shape with the same diameter for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine blades that can be accelerated and fully machined by pressure with the same diameter and the same shape for each stage, and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with turbine rotor blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage, and 5 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Accelerating with pressure + Combined engine with various energy storage cycles, with turbine blades set to approximately the same shape for each stage, with 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group with the same diameter and the same shape for each paragraph, and various energy conservation cycle coalescing engines with 7 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which the same diameter and diameter of each paragraph are provided and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each stage, and 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in heat quantity and mass are set to the same diameter and shape of each stage, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which the turbine blades that can be accelerated and fully processed automatically by the pressure divided and stored in the amount of heat and mass are roughly the same shape for each stage and have four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration + full-automatic machining with pressure divided and stored in heat and mass are made substantially the same shape with the same diameter for each stage and fitted with bolted turbines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blade groups of the same diameter and shape of each stage and fitting bolt assembly turbines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure divided and stored in calorie and mass + various energy storage cycle coalescing engines with turbine rotor blades of the same diameter and shape of each stage and fitted with bolted turbine assembly in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully-automatically processed by the pressure divided and stored in mass or compressed air calorie and mass are provided in 8 stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with 9 stages of turbine bolts with the same diameter and the same shape for each stage of the turbine blades that can be accelerated and fully automated by mass or compressed air heat and mass. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles, the turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure divided into masses have the same diameter and shape of each stage, and are equipped with 10 fitting bolt assembly turbines. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the acceleration and turbine blade groups are arranged in the same shape and the same shape for each stage, and the mating bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with two stages of mating bolt assembly turbines with acceleration / turbine blades grouped in the same diameter and approximately the same shape with pressure divided and stored in mass or compressed air heat quantity and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines, with the turbine blades of the acceleration + fully automatic processing turbines having the same diameter and the same shape for each stage and the fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy conservation cycle coalescing engines with a turbine blade group capable of acceleration + fully automatic machining, with the same diameter and the same shape for each stage, and 5 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage and the fitting bolt assembly turbine is provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with 7 stages of mating bolt assembly turbines with the acceleration + turbine blade group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic processing possible Combined engine with various energy storage cycles, with turbine blades of the same diameter and the same shape for each stage, and 8 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines with turbine rotor blades that can be accelerated by pressure and fully automatic machined, with the same diameter and the same shape for each stage, and 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines with turbine blades that can be accelerated and fully machined by pressure, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Turbine blade group of each turbine with the same diameter and the same shape for each stage, and a combined bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with acceleration and pressure + turbine blades grouped in the same diameter and shape of each stage and fitted bolt assembly turbines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines with the same diameter and the same shape for each paragraph, and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade capable of fully automatic processing Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + combustion gas calorie and mass or compressed air calorie and pressure are stored separately and stored in the turbine + fully automatic machining is possible Various energy conservation cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and five stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 6-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines with 7-stage fitting bolt assembly turbines with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy conservation cycle coalescence engines with 8 stages of fitting bolt assembly turbines, with turbine blades that are accelerated and fully automatic machined by pressure divided and stored in heat and mass and have the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with a turbine blade group that can be accelerated and fully automatically machined by pressure divided and stored in heat quantity and mass, with the same diameter and the same shape for each stage, and with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines in which turbine blades capable of acceleration and full-automatic machining with pressure divided and stored in calorie and mass are made to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescence engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph and with a fitting bolt assembly turbine in one stage with pressure divided and stored in heat and mass. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Various energy storage cycle coalescing engines with acceleration and turbine blade groups of the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which the turbine blades of the turbine that can be accelerated and fully automatic machined by the pressure divided and stored in mass or compressed air calorie and mass are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines in which turbine blades that can be accelerated and fully automated by mass or compressed air heat quantity and mass are stored in four stages with the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Combined with various energy storage cycles in which turbine blades that can be accelerated and fully automated by mass or compressed air calorie and pressure are stored in the same diameter and shape of each stage and fitted with a bolt assembly turbine in five stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescing engines with acceleration / turbine blades grouped in mass or compressed air calorie and mass and stored in six stages with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Various energy storage cycle coalescence engines with acceleration / turbine moving blades grouped into mass or compressed air calorie and mass and having the same diameter and shape of each turbine, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with 8 stages of mating bolt assembly turbines, with the rotor blade groups of the turbine capable of acceleration + fully-automatic machining having the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines in which the turbine blade groups that can be accelerated and fully machined are of the same diameter and the same shape for each stage, and are provided with 9 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. Various energy storage cycle coalescing engines with 10 stages of mating bolt assembly turbines, with turbine blades capable of accelerating + fully automatic machining, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy conservation cycle coalescing engines in which the rotor blade group of the acceleration + turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various energy storage cycle coalescing engines with the acceleration + turbine rotor blade group having the same diameter and the same shape for each paragraph, and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed at the corner of the outer corner of the square turbine to save and use liquid metal + Accelerate by pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in three stages with thrust bearings, bearings, and a rectangular turbine outer casing (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine to save and use liquid metal + Accelerate with pressure divided and stored into combustion gas calorie and mass or compressed air calorie and mass + turbine blade group of turbines capable of fully automatic processing per paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape as thrust bearings, bearings and square turbine outer box (77a) provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine to save and use the liquid metal + Accelerate with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + turbine blade group of turbines capable of fully automatic machining Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in five stages together with thrust bearings and bearings and a rectangular turbine outer casing (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 8 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in 9 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 10 stages together with a type turbine outer box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy storage cycle engines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 3 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 5 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 6 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 7 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engines provided in 8 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in 9 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square type Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in one stage together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square type Various energy storage cycle combined engine provided in two stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in three stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in four stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in five stages together with a type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 6 stages together with a type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 7 stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with the pressure divided into mass or compressed air calorie and mass and the turbine blade group of turbines with the same diameter and the same shape for each stage. ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy storage cycle engines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with the pressure divided into mass or compressed air calorie and mass and the turbine blade group of turbines with the same diameter and the same shape for each stage. ) Combined with various energy conservation cycle engines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and rectangular turbine outer casing (77a ) Combined with various energy storage cycle engines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and rectangular turbine outer casing (77a ) Combined with various energy conservation cycle engines in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) at right angles to square turbine outer box to make rotation direction alternate heat retaining turbine and accelerate liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with combustion gas calorie and mass or compressed air calorie and mass storage + Fully automatic processing possible Turbine blade group with the same diameter and the same shape for each paragraph Thrust of fitting bolt assembly turbine and heat pump Various energy storage cycle coalescence engines provided in three stages together with a bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Acceleration with combustion gas calorie and mass or compressed air calorie and mass storage + Fully automatic machining of turbine blades with the same diameter and shape of each paragraph Various energy storage cycle coalescence engines provided in 4 stages together with thrust bearings, bearings and square turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation and use + Acceleration with the pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of full-automatic machining with the same diameter and the same shape for each stage assembling bolt assembly turbine and heat pump Various energy storage cycle coalescing engines provided in five stages together with thrust bearings, bearings and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided into combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group is set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are thrust bearings and bearings Various energy storage cycle coalescence engine provided in 6 stages together with the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with combustion gas calorie and mass or compressed air calorie and mass storage + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings Various energy storage cycle coalescence engine provided in 7 stages together with the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine for large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + output increasing sphere ( 2E) is accelerated with a small diameter + accelerated with a pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + a fully-automatically processable turbine blade group having a same diameter and substantially the same shape for each stage, Various energy storage cycle coalescing engines with heat pumps installed in three stages together with thrust bearings, bearings and rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine for large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + output increasing sphere ( 2E) is accelerated with a small diameter + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group of turbines capable of full-automatic machining is set to the same diameter and approximately the same shape for each stage. And various energy storage cycle coalescing engines in which a heat pump is provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) liquid metal solar heat engine for large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + output increasing sphere ( 2E) is accelerated with a small diameter + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic machining has the same diameter and shape of each paragraph assembling bolt assembly Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternately heat retaining turbine + Output increasing sphere ( 2E) Accelerate with a small diameter + Accelerate with combustion gas calorie and mass or compressed air calorie and mass + Save turbine turbine blades with the same diameter and shape of each turbine, and thrust the fitting bolt assembly turbine and heat pump Various energy storage cycle coalescence engines provided in 6 stages together with bearings, bearings and rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+出力増大球(2E)を小径として加速する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine for large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + output increasing sphere ( 2E) Accelerate with small diameter + Accelerate with combustion gas calorie and mass or compressed air calorie and mass + Rotate turbine blades with the same diameter and shape of each stage, and thrust the fitting bolt assembly turbine and heat pump Various energy storage cycle coalescence engines provided in 7 stages together with bearings, bearings and rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Acceleration turbine driving with a small output sphere (2E) as a small diameter + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining possible Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in approximately eight stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Acceleration turbine driving with a small output sphere (2E) as a small diameter + Acceleration with combustion gas calorie and mass or compressed air calorie and mass pressure + Fully automatic machining turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in nine stages with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Accelerate turbine drive with small output sphere (2E) as a small diameter + Accelerate with combustion gas calorie and mass or compressed air calorie and mass pressure + Turbine blade group of turbine capable of fully automatic machining per paragraph Various energy storage cycle coalescing engines having a fitting bolt assembly turbine and a heat pump of the same diameter and substantially the same shape, as well as a thrust bearing, a bearing and a rectangular turbine outer box (77a) provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Accelerate turbine drive with small output sphere (2E) as a small diameter + Accelerate with pressure of combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are fitted in the same shape with the same diameter for each paragraph Various energy storage cycle coalescing engines in which a combined bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+出力増大球(2E)を小径として加速タービン駆動する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Accelerate turbine drive with small output sphere (2E) as a small diameter + Accelerate with pressure of combustion gas calorie and mass or compressed air calorie and mass + Turbine blades are fitted in the same shape with the same diameter for each paragraph Various energy storage cycle coalescing engines in which a combined bolt assembly turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corner + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and the same shape for each paragraph Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corners + Accelerated with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic processing is fitted in the same shape with the same diameter for each paragraph Various energy storage cycle coalescing engines in which a combined bolt assembly turbine and a heat pump are provided in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corners. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box The liquid metal is used for ascending and storage provided at the corners + Accelerated by the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with a heat pump provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box The liquid metal is used for ascending and storage provided at the corners + Accelerated by the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with heat pumps provided in two stages together with thrust bearings, bearings and square turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corner + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and the same shape for each paragraph Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corners + Accelerated with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group capable of fully automatic processing is fitted in the same shape with the same diameter for each paragraph Various energy storage cycle coalescing engines in which a combined bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corners. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) ++ Insulation increase sphere raising device (2F) in square turbine outer box The liquid metal is used for ascending and storage provided at the corners + Accelerated by the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines with heat pumps installed in 6 stages together with thrust bearings, bearings and square turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Insulation increase sphere raising device (2F) in square turbine outer box Installed at the corners to save and use liquid metal + Accelerate by pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fitting turbine assembly with turbine rotor blade group with same diameter and shape of each paragraph Various energy storage cycle coalescence engines with heat pumps installed in 7 stages together with thrust bearings, bearings and square turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 8 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in 9 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 10 stages together with a type turbine outer box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy storage cycle engines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 3 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Acceleration with pressure that is divided and stored into mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 5 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 6 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 7 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engines provided in 8 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in 9 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square type Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + turbine blade group that can be fully automatic machined with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and square type Various energy storage cycle coalescence engine provided in one stage together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure that is divided and stored in mass or compressed air calorie and mass + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square type Various energy storage cycle combined engine provided in two stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in three stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in four stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorific value and mass is made into the same shape and shape of the same diameter for each stage. Various energy storage cycle coalescing engines provided in five stages together with a type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 6 stages together with a type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value The turbine blade group of turbines that can be accelerated and fully automated with the pressure divided and stored in mass or compressed air calorie and mass, and with the same diameter and shape of each stage, is fitted with a bolt assembly turbine and heat pump, thrust bearing, bearing and angle Various energy storage cycle coalescing engines provided in 7 stages together with the type turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with the pressure divided into mass or compressed air calorie and mass and the turbine blade group of turbines with the same diameter and the same shape for each stage. ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) And various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy storage cycle engines in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with the pressure divided into mass or compressed air calorie and mass and the turbine blade group of turbines with the same diameter and the same shape for each stage. ) Combined with various energy conservation cycle engines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine outer box (77a ) Combined with various energy conservation cycle engines in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and rectangular turbine outer casing (77a ) Combined with various energy storage cycle engines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal by installing a heat retention increasing ball rising device (2F) at the corner of the square turbine outer casing + Combustion gas calorific value Accelerating with pressure divided and stored in mass or compressed air calorie and mass + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings, bearings and rectangular turbine outer casing (77a ) Combined with various energy conservation cycle engines in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection unit (78S) injection driving force + Insulates and uses the liquid metal at the corners of the square turbine outer box by installing a warming and increasing ball raising device (2F) + Combustion gas calorific value Acceleration with pressure that is divided and stored in mass or compressed air heat quantity and mass + Turbine blades are assembled into bolts with the same diameter and shape of each stage, and heat pumps are thrust bearings, bearings, and rectangular turbine outer casings ( 77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Ascending and using liquid metal + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic processable turbine blade group with same diameter and same shape per stage Various energy storage cycle coalescing engines with heat pumps provided in three stages together with thrust bearings, bearings and square turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) at corner corner of square turbine Ascending and using liquid metal + Accelerating with pressure of combustion gas calorie and mass or compressed air calorie and mass storage + Turbine blade group of turbine that can be fully automatic machined with the same diameter and shape of each paragraph And various energy storage cycle coalescing engines in which a heat pump is provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) at corner corner of square turbine Ascending and using liquid metal + Combustion gas calorie and mass or Compressed air calorie and pressure accelerated by dividing and storing pressure + Turbine blade group capable of fully automatic machining with the same diameter and shape of each paragraph assembling bolt assembly Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) at corner corner of square turbine Uses liquid metal ascending and conserving + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and the same shape for each stage Thrusting bolt assembly turbine and heat pump Various energy storage cycle coalescence engines provided in 6 stages together with bearings, bearings and rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) at corner corner of square turbine Uses liquid metal ascending and conserving + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine rotor blade group with the same diameter and the same shape for each stage Thrusting bolt assembly turbine and heat pump Various energy storage cycle coalescence engines provided in 7 stages together with bearings, bearings and rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same diameter and shape at each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining, with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in five stages together with thrust bearings, bearings and rectangular turbine outer casing (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage. Acceleration by pressure + Fully automatic processing possible Various types of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 8 stages with thrust bearings, bearings and rectangular turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure, have the same diameter and shape of each stage, and are fitted with a bolt assembly turbine and heat pump in 9 stages along with thrust bearings, bearings, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is made to be approximately the same shape for each stage, and fitting bolt assembly turbine and heat pump are provided in 10 stages together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Combined with various energy conservation cycles organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + Fully automatic workable turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat retaining turbine + Heat retention increasing sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass + The turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in seven stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engine provided in 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) And various energy conservation cycle coalescence engines provided in 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in one stage with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored separately in heat quantity and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in two stages together with thrust bearing, bearing and square turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescing engines provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage, and the fitting bolt assembly turbine and heat pump are installed in 8 stages together with thrust bearings, bearings and rectangular turbine outer box (77a). Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Acceleration + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 9 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas heat quantity and mass or compressed air heat quantity and mass Various types of turbine rotor blades capable of acceleration + fully automatic machining are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a), with a bolt assembly turbine and a heat pump having the same diameter and shape of each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used. + The pressure divided and stored in the combustion gas calorie and mass or compressed air calorie and mass Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in one stage together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the acceleration + turbine has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Acceleration by pressure + Fully automatic machining The turbine rotor blade group has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages with thrust bearings, bearings, and the rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine blades that can be accelerated and fully automated by pressure are set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in four stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used. + Divided and stored into combustion gas calorie and mass or compressed air calorie and mass Turbine rotor blade group capable of acceleration + fully automatic machining by pressure is set to be approximately the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter for each stage and fitting bolt assembly Turbine and heat pump are combined in 6 stages with thrust bearings, bearings and rectangular turbine outer box (77a). organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + combustion gas calorie and mass or compressed air calorie and mass are stored separately Accelerating with pressure + Turbine blade group with the same diameter and shape of each stage, Fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Fully automatic machining turbine blade group The various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending and storing. + Acceleration with combustion gas calorie and mass or compressed air calorie and mass stored separately + Turbine blade capable of fully automatic processing Various energy storage cycle coalescing engines in which the group is made into the same shape and the same diameter for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) liquid metal solar thermal engine with large injection propulsion output + horizontal axis (1h) with square turbine outer box at right angle to make rotating direction alternate heat insulation turbine + heat retention increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is stored in an uplifted state. + Acceleration with pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass. Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box, and the liquid metal is used for ascending storage + Acceleration with the pressure divided and stored in combustion gas calorie and mass or compressed air calorie and mass + Turbine blade group in each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Acceleration with pressure stored and divided into calorie and mass + Fully automatic processing possible The turbine blades are of the same shape and shape with the same diameter for each stage The fitting bolt assembly turbine and the heat pump are thrust bearings, bearings and rectangular turbine outer casing (77a) Various energy storage cycle coalescence engines provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air The turbine blade group of the turbine that can be accelerated and fully automatically machined by the pressure divided and stored in the amount of heat and mass is made into the same shape and the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are installed in the thrust bearing, bearing, and square turbine outer box ) Combined with various energy storage cycle engines in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Turbine blades that can be accelerated and fully-automatically processed with pressure divided and stored in the amount of heat and mass are made to have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and rectangular turbine casings ( 77a) Various energy storage cycle coalescence engines provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 6 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Combustion gas heat quantity and mass or compressed air Accelerate with pressure divided and stored in calorie and mass + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerates with mass or compressed air calorie and pressure divided and stored in mass + Fully automatic processing possible Turbine blades are set to the same shape and shape with the same diameter for each stage The bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing, and square turbine Various energy storage cycle coalescence engine provided in 8 stages with box (77a) タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerates by mass or compressed air calorie and pressure divided and stored in mass + turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 9 stages with outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and The turbine blades that can be accelerated and fully-automatically processed with the mass or compressed air heat quantity and mass are stored in the same diameter and approximately the same shape for each stage. The fitting bolt assembly turbine and heat pump are thrust bearings, bearings, and squares. Various energy storage cycle coalescence engines provided in 10 stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward + Driving various types of airplanes in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the rectangular turbine outer box and using the liquid metal for rising storage + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) In addition, various energy conservation cycle coalescence engines provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+燃焼ガス熱量と質量又は圧縮空気熱量と質量に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) in the corner of the outer corner of the square turbine to use the liquid metal ascending and storing + Combustion gas calorific value and Accelerate with mass or compressed air calorie and mass and save pressure + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engines provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in eight stages with a thrust bearing, a bearing, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape, provided in 9 stages together with thrust bearings, bearings and square turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in 10 stages together with thrust bearings, bearings and a rectangular turbine outer box (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in three stages with thrust bearings, bearings, and a rectangular turbine outer casing (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines with fitting bolt assembly turbines and heat pumps having the same diameter and substantially the same shape as thrust bearings, bearings, and a rectangular turbine outer box (77a) in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in five stages together with thrust bearings and bearings and a rectangular turbine outer casing (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are of the same shape and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 8 stages. Various energy conservation cycle coalescence engine established in タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in three stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The rotor blade group of the turbine has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a) in four stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The blades of the turbine have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in five stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Fully automatic processable The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a square turbine outer box (77a) in six stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are almost the same shape for each stage, and the assembly bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 7 stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) 8 Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating The turbine blades of the turbine capable of compressing hot and cold production and fully automatic processing with the same diameter and the same shape for each stage are fitted with a fitting bolt assembly turbine and a heat pump together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engine in 3 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 10 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 5 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 6 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and air production + Turbine blades are almost the same shape for each stage to form a fitting bolt assembly, and heat pumps are provided in 8 stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot and cold air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pumps are provided in 9 stages together with thrust bearings, bearings and rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pump with 10 stages along with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump in two stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled + Fully automatic processable The turbine blades are of the same diameter and shape of each stage, and the bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing or square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed hot and cold manufacturing + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled manufacturing + Turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square type Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Together with various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with a turbine assembly and a heat pump in six stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) with a moving blade group of turbines and a diameter of substantially the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades and the heat pumps are arranged in two stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) with the rotor blades of the turbine + the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 3 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is driven at right angles to square turbine outer box to drive alternating turbines in rotational direction + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heating and cooling production + fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades and the heat pump are installed in a single stage together with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the moving blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in eight stages with a thrust bearing, a bearing, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape, provided in 9 stages together with thrust bearings, bearings and square turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in 10 stages together with thrust bearings, bearings and a rectangular turbine outer box (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in three stages with thrust bearings, bearings, and a rectangular turbine outer casing (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines with fitting bolt assembly turbines and heat pumps having the same diameter and substantially the same shape as thrust bearings, bearings, and a rectangular turbine outer box (77a) in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in five stages together with thrust bearings and bearings and a rectangular turbine outer casing (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are of the same shape and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 8 stages. Various energy conservation cycle coalescence engine established in タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in three stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The rotor blade group of the turbine has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a) in four stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The blades of the turbine have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in five stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Fully automatic processable The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a square turbine outer box (77a) in six stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are almost the same shape for each stage, and the assembly bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 7 stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) 8 Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating The turbine blades of the turbine capable of compressing hot and cold production and fully automatic processing with the same diameter and the same shape for each stage are fitted with a fitting bolt assembly turbine and a heat pump together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engine in 3 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 10 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 5 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 6 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and air production + Turbine blades are almost the same shape for each stage to form a fitting bolt assembly, and heat pumps are provided in 8 stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot and cold air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pumps are provided in 9 stages together with thrust bearings, bearings and rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pump with 10 stages along with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump in two stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled + Fully automatic processable The turbine blades are of the same diameter and shape of each stage, and the bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing or square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed hot and cold manufacturing + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled manufacturing + Turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square type Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Together with various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in eight stages with a thrust bearing, a bearing, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape, provided in 9 stages together with thrust bearings, bearings and square turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in 10 stages together with thrust bearings, bearings and a rectangular turbine outer box (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing possible. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in three stages with thrust bearings, bearings, and a rectangular turbine outer casing (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines with fitting bolt assembly turbines and heat pumps having the same diameter and substantially the same shape as thrust bearings, bearings, and a rectangular turbine outer box (77a) in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in five stages together with thrust bearings and bearings and a rectangular turbine outer casing (77a), each having the same diameter and substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output augmenting sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are of the same shape and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 8 stages. Various energy conservation cycle coalescence engine established in タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in three stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The rotor blade group of the turbine has the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a) in four stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The blades of the turbine have the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer box (77a) in five stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Fully automatic processable The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a square turbine outer box (77a) in six stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Air can be compressed and heated and cooled + Fully automatic processable The turbine blades are almost the same shape for each stage, and the assembly bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and a rectangular turbine outer box (77a) in 7 stages. Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) 8 Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating The turbine blades of the turbine capable of compressing hot and cold manufacturing + fully automatic processing and having the same diameter and the same shape for each stage are fitted with a bolt assembly turbine and a heat pump together with thrust bearings, bearings and a rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating The turbine blades of the turbine capable of compressing hot and cold production and fully automatic processing with the same diameter and the same shape for each stage are fitted with a fitting bolt assembly turbine and a heat pump together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engine in 3 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Turbine blades capable of compressing hot and cold production and fully automatic machining with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescence engine provided in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy storage cycle coalescing engines in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold heat and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump together with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 10 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and cold production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Drives + Drives various flying vessels with united engine injection part (78S) injection driving force + Insulates and uses liquid thermal riser by installing heat-increasing sphere raising device (2F) at corner of outer corner of square turbine + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 5 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 6 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 7 stages Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed and heated air and air production + Turbine blades are almost the same shape for each stage to form a fitting bolt assembly, and heat pumps are provided in 8 stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot and cold air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pumps are provided in 9 stages together with thrust bearings, bearings and rectangular turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + turbine rotor blade group with the same diameter and shape of each stage for assembly bolt assembly, and heat pump with 10 stages along with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various flying ships with united engine injection part (78S) injection propulsion force + Insulates and uses liquid metal rises by installing a heat-retaining and increasing ball raising device (2F) at the corner of the rectangular turbine outer casing + Solar heating Compressed hot / cold air and air production + Turbine blade group with the same diameter and shape of each stage for assembly bolt assembly and heat pump in two stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled + Fully automatic processable The turbine blades are of the same diameter and shape of each stage, and the bolt assembly turbine and heat pump are installed outside the thrust bearing, bearing or square turbine Various energy conservation cycle coalescence engine provided in 3 stages with box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed hot and cold manufacturing + Fully automatic machining turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square turbine Various energy storage cycle coalescence engine provided in 4 stages together with the outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Solar heating air is compressed and heated and cooled manufacturing + Turbine blade group capable of full-automatic processing is made to have the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump as thrust bearing, bearing and square type Various energy storage cycle coalescence engine provided in five stages together with the turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Various energy storage cycle coalescence engines provided in 6 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation use + Compressed and heated solar air heating and cooling + Turbine rotor blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearings and bearings and rectangular turbine outer box (77a) Together with various energy conservation cycle coalescence engine provided in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in eight stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in nine stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade groups of possible turbines have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which groups are arranged in the same shape for each stage, and a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in two stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cool energy production + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 8 stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated Various types of turbine blades and heat pumps with 9 stages in combination with thrust bearings, bearings, and rectangular turbine outer casing (77a), with turbine blades that have the same diameter and the same shape for each stage. Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated The turbine blade group capable of cold-heating manufacturing and fully automatic machining is made to have the same diameter and shape of each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the cooling blades + turbine turbine blade group set to the same diameter and shape of each stage, and fitted bolt assembly turbines and heat pumps with thrust bearings, bearings, and a rectangular turbine outer box (77a) in one stage . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in two stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and approximately the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed and produced with heat and cold + Fully automatic processing possible Various energy storage cycle coalescing engines in which the rotor blade group of a simple turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine and the heat pump are provided in four stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of square turbine outer box and liquid metal is raised and used for storage + Solar heating air is compressed with heat and cold production + Fully automatic processing Various energy storage cycle coalescing engines in which the turbine blade group of possible turbines has the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are arranged in the same shape for each stage and the bolt assembly turbine and the heat pump are provided in six stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and liquid metal is raised and used for storage + Solar heated air is compressed and heated and produced with heat + turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in seven stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Cold energy manufacturing + Fully automatic processing possible Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in three stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various kinds of turbine blades that have the same diameter and almost the same shape for each stage, and are equipped with a fitting bolt assembly turbine and a heat pump in four stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). Energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated A turbine blade group capable of cold-heating manufacturing and fully automatic machining is provided with the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescence engine with a turbine assembly and a heat pump in six stages with thrust bearings, bearings, and a rectangular turbine outer box (77a), with the cooling blade manufacturing + turbine rotor blade group having the same diameter and the same shape for each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines, with the turbine blades and heat pumps installed in 7 stages together with thrust bearings, bearings, and the rectangular turbine outer box (77a), with the rotor blades of the turbine + the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in eight stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in nine stages in substantially the same shape together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Fully automatic machining of turbine blade group for each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in 10 stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a) as substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in one stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines provided with a fitting bolt assembly turbine and a heat pump in four stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in five stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Fully automatic machineable turbine blades Various energy storage cycle coalescing engines in which the groups are divided into substantially the same diameter for each stage and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Fully automatic processing of turbine movement Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in 9 stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + Fully automatic machining of the turbine Various energy storage cycle coalescing engines in which the rotor blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 10 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Turbine blade group for each paragraph Various energy storage cycle coalescing engines having a fitting bolt assembly turbine and heat pump of the same diameter and substantially the same shape as a thrust bearing, a bearing and a rectangular turbine outer box (77a) provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Turbine blade group for each paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape, provided in two stages together with thrust bearings, bearings and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The rotor blades of the turbine have the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in three stages together with thrust bearings, bearings, and the rectangular turbine outer casing (77a) Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in 4 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air The turbine blades capable of compressing hot and cold manufacturing and fully automatic machining are set to the same diameter and the same shape for each stage, and the fitting bolt assembly turbine and heat pump are combined with thrust bearings, bearings, and the rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 6 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump in 7 stages with thrust bearing, bearing and square turbine outer box (77a) Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lift device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in eight stages together with the thrust bearing, the bearing, and the rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in 9 stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heating air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each stage, and a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in a single stage together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and the heat pump are provided in two stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in three stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in four stages in substantially the same shape together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Fully automatic machining of turbine blade group for each paragraph Various energy storage cycle coalescing engines in which fitting bolt assembly turbines and heat pumps are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage. Various energy storage cycle coalescing engines in which a bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used. + Solar heated air is compressed and heated and cooled. + Fully automatic processing is possible. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 8 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescence engines provided with a fitting bolt assembly turbine and a heat pump in 9 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in 10 stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a) as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in a single stage together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which a turbine and a heat pump are provided in two stages together with a thrust bearing, a bearing and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Fully automatic machineable turbine blades Various energy storage cycle coalescing engines in which the groups are made into the same shape and the same diameter for each stage, and the fitting bolt assembly turbine and the heat pump are provided in three stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Fully automatic processing of turbine movement Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage and the fitting bolt assembly turbine and heat pump are provided in four stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + Fully automatic machining of the turbine Various energy storage cycle coalescing engines in which the blade group is substantially the same shape for each paragraph, and the fitting bolt assembly turbine and the heat pump are provided in five stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Turbine blade group for each paragraph Various energy storage cycle coalescing engines having a fitting bolt assembly turbine and a heat pump, which have the same diameter and substantially the same shape, provided in six stages together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Turbine blade group for each paragraph Various energy storage cycle coalescence engines with fitting bolt assembly turbines and heat pumps of the same diameter and substantially the same shape as thrust bearings, bearings, and a rectangular turbine outer box (77a) in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic processing possible The turbine blades are set to the same diameter and shape of each stage, and the fitting bolt assembly turbine and heat pump are arranged in 8 stages together with thrust bearings, bearings and rectangular turbine outer casing (77a). Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Fully automatic machining of turbine blades with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with 9 stages with thrust bearing, bearing and square turbine outer box (77a) Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air A turbine blade group capable of full-automatic machining and compression hot / cold heat production is set to have the same diameter and shape of each stage, and a fitting bolt assembly turbine and a heat pump are installed together with a thrust bearing, a bearing and a rectangular turbine outer box (77a). Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in one stage Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Turbine blade group with the same diameter and shape of each stage, fitting bolt assembly turbine and heat pump with thrust bearing, bearing and square turbine outer box (77a) in two stages Conservation cycle coalescence organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each stage, and the fitting bolt assembly turbine and heat pump are provided in three stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and stored + Solar heated air is compressed and heated and cooled + Turbine capable of fully automatic processing Various energy storage cycle coalescing engines in which the rotor blade group of each stage is substantially the same shape for each stage, and the fitting bolt assembly turbine and the heat pump are provided in four stages together with the thrust bearing, the bearing and the rectangular turbine outer casing (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Fully automatic processing is possible Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph, and the fitting bolt assembly turbine and heat pump are provided in five stages together with thrust bearings, bearings, and a rectangular turbine outer box (77a). タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Solar heating air is compressed and heated and cooled + The turbine blades Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine and heat pump are provided in six stages together with thrust bearings, bearings, and a rectangular turbine outer casing (77a) with the same diameter and substantially the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービン及び熱ポンプを推力軸受や軸受や角型タービン外箱(77a)と共に7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection section (78S) Liquid metal solar engine that makes large propulsion propulsion output + Accelerating the output sphere (2E) downward by gravity acceleration Turbine drive + Combined engine injection section (78S ) Drives the propulsion force + Insulates and heats up ball riser (2F) at the corner of the square turbine outer casing and uses the liquid metal to save and use + Solar heating air is compressed hot and cold manufacturing + Turbine blade group Various energy storage cycle coalescing engines in which a fitting bolt assembly turbine and a heat pump are provided in seven stages together with a thrust bearing, a bearing, and a rectangular turbine outer casing (77a) as each paragraph having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine to save and use liquid metal + solar heated air is compressed and heated and cooled + liquid metal is accelerated and the turbine blades equipped with a heat retention device are the same diameter per paragraph Various energy storage cycle coalescing engines with approximately the same shape and 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed at the corner of the outer corner of the square turbine, and the liquid metal is used for storage and storage. + Solar heating air is compressed and heated and cooled. Various energy storage cycle coalescing engines with fitting bolt assembly turbines in 9 stages with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed at the corner of the outer casing of the square turbine, and the liquid metal is used for storage and storage. + Solar heated air is compressed and heated and cooled. + The rotor blade group of the turbine equipped with the liquid metal acceleration drive is kept the same diameter for each paragraph. Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed in the corner of the outer corner of the square turbine to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is heat-accelerated and heat turbine drive blade group equipped with turbines Various energy storage cycle coalescing engines with a fitting bolt assembly turbine arranged in one stage and having substantially the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+燃料費僅少CO2排気僅少合体機関噴射部(78S)で噴射推進出力増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection unit (78S) Liquid metal solar engine to make large injection propulsion output + fuel cost is small CO2 exhaust gas small coalescence engine injection unit (78S) injection propulsion output increase + heat retention increase ball lift device (2F) Is installed at the corner of the outer corner of the square turbine to save and use the liquid metal + Solar heated air is compressed and heated and cooled + The liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages with approximately the same diameter. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + The liquid metal is accelerated and heated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines having the same diameter are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Heating / cooling production with intake air path length lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + The liquid metal is accelerated by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and sunlight to produce heat and cold + Heat retention increasing sphere lift device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + Liquid metal acceleration drive heat retention device Various energy storage cycle coalescing engines in which the blades of the turbines provided have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Heating / cooling production with intake air path length lens and sunlight + Heat retention increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used for storage + Liquid metal is heated for heat acceleration Various energy storage cycle coalescing engines in which the turbine blades equipped with the apparatus have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Heating / cooling production with intake air path length lens and sunlight + Heat retention sphere raising device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is lifted and used for storage + Liquid metal is heated by mass acceleration drive Various energy storage cycle coalescing engines in which the rotor blade group of the turbine equipped with the apparatus is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + The liquid metal is accelerated and heated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines having the same diameter are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+より重い物質を真空方向加速して発電量増大を保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けて1000倍発電量を狙う各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + Accelerates heavier substances in the vacuum direction Various energy storage cycle coalescence engines aiming at 1000 times power generation by providing a turbine rotor blade group equipped with a heat retaining device with the same diameter and substantially the same shape for each stage, and providing 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drive + Intake air path length lens and sunlight to produce heat and cold + Heat retention increasing sphere lift device (2F) is installed at the corner of the square turbine outer box and the liquid metal is lifted and used for storage + Liquid metal acceleration drive heat retention device Various energy storage cycle coalescing engines in which the moving blade group of the provided turbine is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Heating / cooling production with intake air path length lens and sunlight + Heat retention increasing sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used for storage + Liquid metal is heated for heat acceleration Various energy storage cycle coalescing engines in which the blades of the turbine equipped with the apparatus have substantially the same shape and the same diameter for each stage and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Heating / cooling production with intake air path length lens and sunlight + Heat retention sphere raising device (2F) is installed in the corner of the outer corner of the square turbine, and liquid metal is lifted and used for storage + Liquid metal is heated by mass acceleration drive Various energy storage cycle coalescing engines in which the rotor blade group of the turbine equipped with the apparatus is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. As a combination engine of various energy storage cycles with three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines that are approximately the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engine with 5 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with 6 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbines in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with a mating bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescence engine with two stages of fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in three stages as substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines that are approximately the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy conservation cycle coalescing engines with approximately the same shape and 5 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines that have six stages of fitting bolt assembly turbines that are approximately the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in seven stages as substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engine with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engines with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engines with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engine with a mating bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engine with two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with fitting bolt assembly turbines in three stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with fitting bolt assembly turbines in four stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbines in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with 6 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbines in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with fitting bolt assembly turbines in 9 stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with two fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is lifted and used for storage + Solar heated air is compressed and heated and cooled + Heated by liquid metal acceleration drive Assembling bolt assembly with turbine blades having the same diameter for each stage as the same diameter and approximately the same shape for each stage. Combined engine with various energy storage cycles as a turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above-mentioned heat retaining device have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbine equipped with the above heat retaining device have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. + Solar heating air is compressed and heated and produced by cooling + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in three stages with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage. + Solar heated air is compressed and heated and cooled, and the turbine blade is equipped with a heat retaining device that accelerates the liquid metal by mass. Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in five stages with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines with the same diameter and diameter of each paragraph, and with 6 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines, with the same diameter and diameter of each paragraph, and 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines, with turbine blades equipped with a thermal insulation manufacturing + heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation acceleration drive for heat production of liquid metal + liquid metal are provided in a single stage with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by cold heat + liquid metal mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy combined cycle engine with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and drives liquid metal with the same diameter and shape for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device for accelerating and driving liquid metal by mass with the same diameter and the same shape for each stage, and four bolted turbine assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device that drives a liquid metal to accelerate the calorie of heat, with the same diameter and the same shape for each stage, and six bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device for mass acceleration drive of liquid metal, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device have substantially the same diameter and shape as each stage, and are provided with eight fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the turbine equipped with the apparatus is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the blades of the turbine equipped with the above heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines with fitting bolt assembly turbines in 9 stages each having the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines, each having the same diameter and substantially the same shape, and 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine is provided in one stage with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in two stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation devices having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines, with the turbine blades equipped with a thermal insulation manufacturing + thermal insulation device that accelerates liquid metal by mass and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are set to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation device that is driven by cold heat + liquid metal heat-acceleration drive are provided in six stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by refrigeration and mass acceleration of liquid metal are provided in seven stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device for accelerating and driving liquid metal with the same diameter and shape of each stage, and with 8 bolted fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage, and fitted bolt assembly turbines in 9 stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in 10 stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device that accelerates the heat quantity of liquid metal, with the same diameter and shape of each turbine, and a single bolted turbine assembly. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy storage cycle coalescing engine with turbine rotor blades equipped with a heat retaining device for mass acceleration drive of the same shape, with the same diameter and the same shape for each stage, and two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used for storage + Solar heated air is compressed and heated and cooled + Insulated liquid metal acceleration Various energy storage cycle coalescing engines in which the turbine blades equipped with the apparatus have substantially the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above-mentioned heat retaining device have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbine equipped with the above heat retaining device have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. + Solar heating air is compressed and heated and produced by cooling + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in three stages with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage. + Solar heated air is compressed and heated and cooled, and the turbine blade is equipped with a heat retaining device that accelerates the liquid metal by mass. Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in five stages with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines with the same diameter and diameter of each paragraph, and with 6 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines, with the same diameter and diameter of each paragraph, and 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines, with turbine blades equipped with a thermal insulation manufacturing + heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation acceleration drive for heat production of liquid metal + liquid metal are provided in a single stage with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by cold heat + liquid metal mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy combined cycle engine with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and drives liquid metal with the same diameter and shape for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device for accelerating and driving liquid metal by mass with the same diameter and the same shape for each stage, and four bolted turbine assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device that drives a liquid metal to accelerate the calorie of heat, with the same diameter and the same shape for each stage, and six bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device for mass acceleration drive of liquid metal, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device have substantially the same diameter and shape as each stage, and are provided with eight fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the turbine equipped with the apparatus is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the blades of the turbine equipped with the above heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage. + Solar heated air is compressed and heated and cooled, and the turbine blade is equipped with a heat retaining device that accelerates the liquid metal by mass. Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines, each having the same diameter and substantially the same shape, and 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine is provided in one stage with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in two stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation devices having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines, with the turbine blades equipped with a thermal insulation manufacturing + thermal insulation device that accelerates liquid metal by mass and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are set to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation device that is driven by cold heat + liquid metal heat-acceleration drive are provided in six stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by refrigeration and mass acceleration of liquid metal are provided in seven stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device for accelerating and driving liquid metal with the same diameter and shape of each stage, and with 8 bolted fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage, and fitted bolt assembly turbines in 9 stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in 10 stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device that accelerates the heat quantity of liquid metal, with the same diameter and shape of each turbine, and a single bolted turbine assembly. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy storage cycle coalescing engine with turbine rotor blades equipped with a heat retaining device for mass acceleration drive of the same shape, with the same diameter and the same shape for each stage, and two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used for storage + Solar heated air is compressed and heated and cooled + Insulated liquid metal acceleration Various energy storage cycle coalescing engines in which the turbine blades equipped with the apparatus have substantially the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above-mentioned heat retaining device have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbine equipped with the above heat retaining device have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. + Solar heating air is compressed and heated and produced by cooling + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in three stages with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage. + Solar heated air is compressed and heated and cooled, and the turbine blade is equipped with a heat retaining device that accelerates the liquid metal by mass. Various energy storage cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in five stages with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines with the same diameter and diameter of each paragraph, and with 6 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines, with the same diameter and diameter of each paragraph, and 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation group having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines, with turbine blades equipped with a thermal insulation manufacturing + heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation acceleration drive for heat production of liquid metal + liquid metal are provided in a single stage with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by cold heat + liquid metal mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy combined cycle engine with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and drives liquid metal with the same diameter and shape for each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device for accelerating and driving liquid metal by mass with the same diameter and the same shape for each stage, and four bolted turbine assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device that drives a liquid metal to accelerate the calorie of heat, with the same diameter and the same shape for each stage, and six bolted turbine assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device for mass acceleration drive of liquid metal, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device have substantially the same diameter and shape as each stage, and are provided with eight fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and heats up sphere lift device (2F) at the corner of the square turbine outer box and uses the liquid metal ascends and saves it + Compresses and heats the solar heated air + Accelerates the liquid metal by mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device to be driven have substantially the same shape and the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is lifted and used. Various energy storage cycle coalescing engines in which the rotor blade group of the turbine equipped with the apparatus is substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the blades of the turbine equipped with the above heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heated air is compressed with heat and cold production + Liquid metal is accelerated Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the outer corner of the square turbine, and liquid metal is lifted and used. + Solar heating air is compressed and heated and produced by cooling + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere rising device (2F) is installed at the corner of the square turbine outer box and liquid metal is lifted and used for storage + Solar heating air is compressed and heated and cold production + liquid metal is calorie Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same shape and diameter for each stage, and are provided with six bolt-fitting assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box, and liquid metal is raised and used for storage + Solar heating air is compressed and heated and cold production + Liquid metal is mass Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage. + Solar heated air is compressed and heated and cooled, and the turbine blade is equipped with a heat retaining device that accelerates the liquid metal by mass. Various energy conservation cycle coalescing engines with groups of approximately the same diameter and the same shape for each paragraph and provided with 9 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal accelerated drive heat insulation group of turbine blades Various energy storage cycle coalescing engines, each having the same diameter and substantially the same shape, and 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed in the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device that drives the liquid metal to accelerate heat. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbine is provided in one stage with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is mass-accelerated and driven. Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in two stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines, with the rotor blades of turbines equipped with heat insulation and liquid metal accelerating drive heat insulation devices having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines, with the turbine blades equipped with a thermal insulation manufacturing + thermal insulation device that accelerates liquid metal by mass and having the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which turbine blades equipped with cold heat production + liquid metal acceleration drive heat retaining device are set to have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat insulation device that is driven by cold heat + liquid metal heat-acceleration drive are provided in six stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and used for storage + Solar heating air is compressed and heated Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that is driven by refrigeration and mass acceleration of liquid metal are provided in seven stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Various energy storage cycle coalescing engines with a turbine blade group equipped with a heat retaining device for accelerating and driving liquid metal with the same diameter and shape of each stage, and with 8 bolted fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed heat and cold production + Combined engine with various energy storage cycles, with turbine blades equipped with a heat retaining device that accelerates liquid metal by mass, with the same diameter and shape of each stage, and fitted bolt assembly turbines in 9 stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Various energy storage cycle coalescing engines in which the turbine blades equipped with compression heat and cold production + liquid metal acceleration drive heat retention device are arranged in 10 stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold production + Liquid energy storage cycle coalescing engine with turbine blades equipped with a heat retaining device that accelerates the heat quantity of liquid metal, with the same diameter and shape of each turbine, and a single bolted turbine assembly. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various aircrafts in the combined engine injection part (78S) injection driving force + Insulating and increasing ball-lifting device (2F) in the corner of the outer corner of the square turbine + Liquid metal is used for rising storage + Solar heating air Compressed hot and cold manufacturing + Liquid energy storage cycle coalescing engine with turbine rotor blades equipped with a heat retaining device for mass acceleration drive of the same shape, with the same diameter and the same shape for each stage, and two fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated and driven Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device have substantially the same diameter and the same shape for each paragraph, and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+より重い物質を真空方向加速して発電量増大を保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けて1000倍発電量を狙う各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled + The heavier material is in the vacuum direction Various energy storage cycle coalescing engines aiming at 1000 times power generation by accelerating and increasing the power generation amount by setting the turbine blades equipped with a heat retaining device to the same diameter and shape of each stage and providing four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injecting propulsion force driving + Insulating sphere increasing device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used for storage + Solar heated air is compressed and heated and cooled + Insulated liquid metal acceleration Various energy storage cycle coalescing engines in which the turbine blades equipped with the apparatus have substantially the same diameter and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion driving + Insulating sphere increasing device (2F) installed at corner of outer corner of square turbine to use and store liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is accelerated Various energy storage cycle coalescing engines in which the turbine blades equipped with the above-mentioned heat retaining device have the same diameter and substantially the same shape for each paragraph, and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driving propulsion force + Insulating and increasing ball riser (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Solar heated air is compressed and heated and cooled + Liquid metal is mass accelerated Various energy storage cycle coalescing engines in which the rotor blade groups of the turbine equipped with the above heat retaining device have the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Insulation increase sphere raising device (2F) in square turbine outer box The liquid metal is stored and used at the corners. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device for accelerating the liquid metal are fitted into the same diameter and shape of each stage. Various energy storage cycle coalescing engines with 8 stages of assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corner + Solar heated air is compressed and heated and cooled + The turbine blades equipped with a heat retaining device that accelerates the liquid metal by mass are fitted with the same diameter and the same shape for each paragraph Various energy storage cycle coalescing engines with 9 stages of combined bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Assembling bolt assembly with the same diameter and the same shape for each stage of the turbine blades equipped with the heat retaining device of the liquid metal acceleration drive. Various energy storage cycle coalescence engine with 10 stages of turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at corners + Solar heated air is compressed and heated and cooled manufacturing + Turbine blades equipped with a heat retaining device that drives liquid metal with heat acceleration are fitted with the same diameter and shape of each paragraph Various energy storage cycle coalescing engine with bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at corners + Solar heated air is compressed and heated and cooled + Liquid turbine is fitted with turbine blades equipped with a heat-insulating device that accelerates mass acceleration with the same diameter for each paragraph Various energy storage cycle coalescing engine with two stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Insulation increase sphere raising device (2F) in square turbine outer box The liquid metal is stored and used at the corners. + Solar heated air is compressed and heated and cooled. + The moving blades of the turbine equipped with a heat retaining device for accelerating the liquid metal are fitted into the same diameter and shape of each stage. Various energy storage cycle coalescence engine with assembly turbines in 3 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at the corner + Solar heated air is compressed and heated and cooled + The turbine blades equipped with a heat retaining device that accelerates the liquid metal by mass are fitted with the same diameter and the same shape for each paragraph Various energy storage cycle coalescing engine with a combined bolt assembly turbine in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Assembling bolt assembly with the same diameter and the same shape for each stage of the turbine blades equipped with the heat retaining device of the liquid metal acceleration drive. Various energy storage cycle coalescence engine with 5 stages of turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at corners + Solar heated air is compressed and heated and cooled manufacturing + Turbine blades equipped with a heat retaining device that drives liquid metal with heat acceleration are fitted with the same diameter and shape of each paragraph Various energy storage cycle coalescing engines with 6 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple-drive short-time coalescence engine injection part (78S) liquid metal solar engine for large injection propulsion output + configuration and method for accelerating output increase sphere (2E) + heat retention increase sphere raising device (2F) in square turbine outer box Liquid metal is stored and used at corners + Solar heated air is compressed and heated and cooled + Liquid turbine is fitted with turbine blades equipped with a heat-insulating device that accelerates mass acceleration with the same diameter for each paragraph Various energy storage cycle coalescing engines with 7 stages of bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines that are approximately the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engines with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with two fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. As a combination engine of various energy storage cycles with three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with four fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with 5 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. Various energy storage cycle coalescing engines with 6 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The rotor blade group of the turbine equipped with a heat retaining device that accelerates the liquid metal is roughly the same shape for each paragraph. As a combination engine of various energy storage cycles with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy conservation cycle coalescing engines with approximately the same shape and 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with 9 stages of fitting bolt assembly turbines that are approximately the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with approximately 10 identically fitted bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in one stage as substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine + turbine rotor blade group equipped with a heat retaining device that accelerates liquid metal by mass is the same diameter per paragraph Various energy storage cycle coalescing engines with fitting bolt assembly turbines arranged in two stages as substantially the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy conservation cycle coalescing engines with three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engines with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engine with 5 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescing engines with 6 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat, divided into compressed air calorie pressure and mass pressure, and each turbine is driven. Various energy storage cycle coalescence engine with fitting bolt assembly turbine in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with fitting bolt assembly turbines in 9 stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with 10 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and divided into compressed air calorie pressure and mass pressure to drive each turbine. + The turbine blades equipped with a heat retaining device that drives the liquid metal to heat are accelerated. Various energy storage cycle coalescing engines with two fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with fitting bolt assembly turbines in three stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with fitting bolt assembly turbines in four stages as the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbines in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with 6 stages of fitting bolt assembly turbines in the same shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight The air is heated and compressed to recover heat and stored separately in compressed air calorie pressure and mass pressure to drive each turbine + turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive Various energy storage cycle coalescing engines with the same type of fitting bolt assembly turbines in 7 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight Compressed heat recovered by heating and compressing heat, and divided and stored into compressed air calorie pressure and mass pressure to drive each turbine. Various energy storage cycle coalescing engine with 8 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight Compressed heat recovered by heating and compressing heat, and divided and stored into compressed air calorie pressure and mass pressure to drive each turbine. Various energy conservation cycle coalescing engines with 9 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight Compressed heat recovered by heating and compressing heat, and divided and stored into compressed air calorie pressure and mass pressure to drive each turbine. Various energy conservation cycle coalescing engines with 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight Compressed heat recovered by heating and compressing heat, and divided and stored into compressed air calorie pressure and mass pressure to drive each turbine. Various energy storage cycle coalescing engines with one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光で空気を加熱圧縮熱回収して圧縮空気熱量圧力と質量圧力に分割保存して夫々のタービンを駆動する+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward + Driving various flying vessels with united engine injection part (78S) injection driving force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for rising storage + sunlight Compressed heat recovered by heating and compressing heat, and divided and stored into compressed air calorie pressure and mass pressure to drive each turbine. Various energy storage cycle coalescing engines with two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Ascending and using liquid metal + Acceleration with pressure divided and stored in calorie speed and mass speed + Turbine blade group equipped with heat retention device that accelerates liquid metal and moving the rotor blade group with the same diameter and shape of each paragraph Various energy conservation cycle coalescence engine with three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Liquid metal is used for ascending storage + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal by mass Various energy storage cycle coalescing engine with assembly turbine in 4 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Ascending and using liquid metal + Accelerating with pressure divided and stored in calorie speed and mass speed + Turbine blades equipped with a heat retaining device for liquid metal acceleration drive with the same diameter and shape of each stage as a fitting bolt assembly turbine Various energy storage cycle coalescence engine provided in 5 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Ascending and using liquid metal + Accelerating with pressure that is divided and stored in calorie speed and mass speed + Assembling bolt assembly with turbine blades equipped with a heat retention device that drives liquid metal in calorie acceleration with the same diameter and shape of each stage Various energy conservation cycle coalescence engine with 6 stages of turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差を可能な限り上昇+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat increase ball riser (2F) raises the head as much as possible + Heat increase ball riser (2F) is installed at the corner of the square turbine outer box Ascending and using liquid metal + Accelerating with pressure that is divided and stored in calorie velocity and mass velocity + Assembling bolt assembly with turbine blades equipped with a heat retaining device that drives mass acceleration of mass and mass of liquid metal in each paragraph Various energy storage cycle coalescing engine with 7 stages of turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing. Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with a heat retaining device that drives the liquid metal mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive rotating turbine in alternate direction of rotation The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive rotating turbine in alternate direction of rotation An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive rotating turbine in alternate direction of rotation Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive rotating turbine in alternate direction of rotation The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする++保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + Horizontal axis (1h) is driven with square turbine outer box at right angle to drive rotating turbine in alternate direction of rotation The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+太陽光加熱空気を圧縮温熱と冷熱製造+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is raised and stored. + Solar heated air is compressed and heated and cooled. + Liquid metal is accelerated and driven. Various energy storage cycle coalescing engines with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing. Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Accelerating with pressure + turbine blade group of turbines having the same diameter and same shape for each stage as a fitting bolt-assembled turbine. Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを38多段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with 38 multistage fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored, and a liquid metal acceleration drive. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing. Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the blades of the turbines provided have substantially the same shape for each stage and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulator that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the moving blade groups of the turbines provided are substantially the same shape for each stage and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulation device that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are of the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with turbine blades equipped with a heat retention device that accelerates and saves liquid metal by acceleration and divided into mass speeds, and has eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with 10 stages of mating bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device that is driven by mass-accelerated pressure + liquid metal and mass-accelerated drive, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with three stages of fitting bolt assembly turbines, with the turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal divided and stored at the mass velocity, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with four stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal by acceleration and liquid metal acceleration, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with the turbine blades equipped with heat insulation that accelerates with the pressure divided and stored in the mass velocity and the heat retaining device that accelerates the liquid metal, each stage has the same diameter and approximately the same shape, and the fitting bolt assembly turbine is provided in five stages. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and drives liquid metal by acceleration and divided into mass speeds are provided with 6 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with 7 stages of mating bolt assembly turbines with turbine blades equipped with a heat insulation device that accelerates with the pressure divided and stored in mass velocity and a heat retention device that accelerates the liquid metal and has the same diameter for each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + turbine blades equipped with a heat retaining device for accelerating liquid metal with mass, each stage has the same diameter and approximately the same shape, and various types of energy storage with fitting bolt assembly turbines in 8 stages Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Accelerates with pressure divided and stored at mass speed + Saves energy by providing turbine bolts with a heat retaining device for accelerating liquid metal by mass with the same diameter and the same shape for each paragraph and 10 mating bolt assembly turbines Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and the same shape as each stage. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal by mass Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines with turbine blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure, with the same diameter and the same shape for each stage, and three bolted assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with four stages of fitting bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are set to have the same diameter and shape of each stage, and are provided with five stages of fitting bolt assembly turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are arranged in substantially the same shape for each stage, and are provided with six bolted turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescence engines with turbine rotor blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-divided storage, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass speed + Various energy storage cycles in which turbine blades equipped with a heat retaining device that drives liquid metal with heat quantity acceleration are set to have the same diameter and shape of each stage, and the fitting bolt assembly turbine is provided in 8 stages Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass velocity + Various energy conservation cycles in which turbine blades equipped with a heat retaining device for liquid metal heat acceleration drive are arranged in the same shape with the same diameter and shape for each stage, and are equipped with 9 fitting bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with 10 stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided by mass velocity, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided into mass speeds, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and mass-accelerated are kept in the same diameter and shape of each stage, and are fitted with three bolted assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and stored in a mass speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-accelerated pressure are divided into mass velocities, and the rotor blades of each turbine are of the same shape and shape with the same diameter for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven with mass-accelerated pressure are divided into mass velocities, and the turbine blades are substantially the same shape for each stage and are fitted in six stages. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that drives the acceleration of the liquid metal by mass acceleration and divided into mass velocities are provided with 7 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressure divided and stored at mass speed are substantially the same shape for each stage, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressure divided and stored at mass speed are substantially the same shape for each stage, and a fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at a mass speed are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure that is divided and stored in calorie speed and mass speed + Liquid metal accelerating turbine blades equipped with heat insulation device are made to have the same diameter and shape of each stage in three stages. Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Storage and use + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Turbine blade group equipped with a heat retaining device that accelerates liquid metal by mass Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preserving use + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Turbine blades equipped with a heat retention device driven by liquid metal acceleration, with the same diameter and shape of each stage, and fitting bolt assembly turbines in 5 stages Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Liquid metal is heated and heat turbine acceleration turbine blades equipped with heat insulation acceleration, each stage has the same diameter and approximately the same shape, fitting bolt assembly turbine 6 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Seven stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive with the same diameter and shape of each paragraph Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the blades of the turbines provided have substantially the same shape for each stage and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulator that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the moving blade groups of the turbines provided are substantially the same shape for each stage and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulation device that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are of the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with turbine blades equipped with a heat retention device that accelerates and saves liquid metal by acceleration and divided into mass speeds, and has eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with 10 stages of mating bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device that is driven by mass-accelerated pressure + liquid metal and mass-accelerated drive, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with three stages of fitting bolt assembly turbines, with the turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal divided and stored at the mass velocity, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with four stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal by acceleration and liquid metal acceleration, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with the turbine blades equipped with heat insulation that accelerates with the pressure divided and stored in the mass velocity and the heat retaining device that accelerates the liquid metal, each stage has the same diameter and approximately the same shape, and the fitting bolt assembly turbine is provided in five stages. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and drives liquid metal by acceleration and divided into mass speeds are provided with 6 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with 7 stages of mating bolt assembly turbines with turbine blades equipped with a heat insulation device that accelerates with the pressure divided and stored in mass velocity and a heat retention device that accelerates the liquid metal and has the same diameter for each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + turbine blades equipped with a heat retaining device for accelerating liquid metal with mass, each stage has the same diameter and approximately the same shape, and various types of energy storage with fitting bolt assembly turbines in 8 stages Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Accelerates with pressure divided and stored at mass speed + Saves energy by providing turbine bolts with a heat retaining device for accelerating liquid metal by mass with the same diameter and the same shape for each paragraph and 10 mating bolt assembly turbines Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and the same shape as each stage. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal by mass Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines with turbine blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure, with the same diameter and the same shape for each stage, and three bolted assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with four stages of fitting bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are set to have the same diameter and shape of each stage, and are provided with five stages of fitting bolt assembly turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are arranged in substantially the same shape for each stage, and are provided with six bolted turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescence engines with turbine rotor blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-divided storage, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass speed + Various energy storage cycles in which turbine blades equipped with a heat retaining device that drives liquid metal with heat quantity acceleration are set to have the same diameter and shape of each stage, and the fitting bolt assembly turbine is provided in 8 stages Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass velocity + Various energy conservation cycles in which turbine blades equipped with a heat retaining device for liquid metal heat acceleration drive are arranged in the same shape with the same diameter and shape for each stage, and are equipped with 9 fitting bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with 10 stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided by mass velocity, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided into mass speeds, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and mass-accelerated are kept in the same diameter and shape of each stage, and are fitted with three bolted assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and stored in a mass speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-accelerated pressure are divided into mass velocities, and the rotor blades of each turbine are of the same shape and shape with the same diameter for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven with mass-accelerated pressure are divided into mass velocities, and the turbine blades are substantially the same shape for each stage and are fitted in six stages. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that drives the acceleration of the liquid metal by mass acceleration and divided into mass velocities are provided with 7 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressure divided and stored at mass speed are substantially the same shape for each stage, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressure divided and stored at mass speed are substantially the same shape for each stage, and a fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at a mass speed are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure that is divided and stored in calorie speed and mass speed + Liquid metal accelerating turbine blades equipped with heat insulation device are made to have the same diameter and shape of each stage in three stages. Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Storage and use + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Turbine blade group equipped with a heat retaining device that accelerates liquid metal by mass Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preserving use + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Turbine blades equipped with a heat retention device driven by liquid metal acceleration, with the same diameter and shape of each stage, and fitting bolt assembly turbines in 5 stages Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Liquid metal is heated and heat turbine acceleration turbine blades equipped with heat insulation acceleration, each stage has the same diameter and approximately the same shape, fitting bolt assembly turbine 6 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Seven stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive with the same diameter and shape of each paragraph Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+タービンを46段に設けて液体鉛合金を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+タービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンとした各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Turbine is installed in 46 stages, liquid lead alloy is accelerated downward + Intake air path length lens and solar heat Refrigeration manufacturing + Insulation sphere raising device (2F) installed at corner of outer corner of rectangular turbine, liquid metal is raised and stored and used + Accelerated by heat stored separately in calorie speed and mass speed + Turbine blade group in each stage Various energy storage cycle coalescing engines with fitting bolt assembly turbines with the same diameter and shape. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the blades of the turbines provided have substantially the same shape for each stage and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in 10 stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulator that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in two stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines in which turbine blade groups are substantially the same shape for each paragraph, and fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere lifting device (2F) is installed at the corner of the square turbine outer box to use and store liquid metal. + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Heat insulation device that accelerates liquid metal by mass Various energy storage cycle coalescing engines in which the moving blade groups of the turbines provided are substantially the same shape for each stage and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A heat retention increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Turbine equipped with a heat retaining device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of each stage are of the same shape and the same shape for each stage, and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming-increasing sphere raising device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + equipped with a heat insulation device that drives the liquid metal to calorie acceleration Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are of the same shape and shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in six stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を加速する構成や方法+吸入空気路長レンズと太陽光で温熱冷熱製造する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar engine for large injection propulsion output + Configuration and method for accelerating output increase sphere (2E) + Intake air path length lens and solar heating / cooling manufacture with sunlight + A warming and increasing ball lifting device (2F) is installed at the corner of the square turbine outer box, and the liquid metal is lifted and used. + Accelerated by the pressure divided and stored in the calorie speed and the mass speed. Various energy storage cycle coalescing engines in which the rotor blade groups of the turbines are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in seven stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with turbine blades equipped with a heat retention device that accelerates and saves liquid metal by acceleration and divided into mass speeds, and has eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with 10 stages of mating bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device that is driven by mass-accelerated pressure + liquid metal and mass-accelerated drive, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with three stages of fitting bolt assembly turbines, with the turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal divided and stored at the mass velocity, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with four stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device that accelerates and saves the liquid metal by acceleration and liquid metal acceleration, and has the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles, with the turbine blades equipped with heat insulation that accelerates with the pressure divided and stored in the mass velocity and the heat retaining device that accelerates the liquid metal, each stage has the same diameter and approximately the same shape, and the fitting bolt assembly turbine is provided in five stages. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and drives liquid metal by acceleration and divided into mass speeds are provided with 6 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Combined with various energy storage cycles with 7 stages of mating bolt assembly turbines with turbine blades equipped with a heat insulation device that accelerates with the pressure divided and stored in mass velocity and a heat retention device that accelerates the liquid metal and has the same diameter for each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + turbine blades equipped with a heat retaining device for accelerating liquid metal with mass, each stage has the same diameter and approximately the same shape, and various types of energy storage with fitting bolt assembly turbines in 8 stages Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and shape, and has 9 stages of fitting bolt assembly turbines. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Accelerates with pressure divided and stored at mass speed + Saves energy by providing turbine bolts with a heat retaining device for accelerating liquid metal by mass with the same diameter and the same shape for each paragraph and 10 mating bolt assembly turbines Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal with mass, each stage has the same diameter and the same shape as each stage. Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored at mass velocity + Turbine blades equipped with a heat retaining device that accelerates liquid metal by mass Cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines with turbine blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure, with the same diameter and the same shape for each stage, and three bolted assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by mass-split pressure are provided with four stages of fitting bolt assembly turbines with the same diameter and shape of each stage. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are set to have the same diameter and shape of each stage, and are provided with five stages of fitting bolt assembly turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by mass-split pressure are arranged in substantially the same shape for each stage, and are provided with six bolted turbines. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescence engines with turbine rotor blades equipped with heat retention device driven by acceleration and liquid metal acceleration driven by mass-divided storage, with the same diameter and the same shape for each stage, and with the fitting bolt assembly turbine in seven stages . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine with large injection propulsion output + Horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat insulation turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass speed + Various energy storage cycles in which turbine blades equipped with a heat retaining device that drives liquid metal with heat quantity acceleration are set to have the same diameter and shape of each stage, and the fitting bolt assembly turbine is provided in 8 stages Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Acceleration with pressure divided and stored in mass velocity + Various energy conservation cycles in which turbine blades equipped with a heat retaining device for liquid metal heat acceleration drive are arranged in the same shape with the same diameter and shape for each stage, and are equipped with 9 fitting bolt assembly turbines Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with 10 stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided by mass velocity, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and heats the liquid metal in a heat-acceleration drive with the pressure divided and stored in the mass velocity are arranged in the same shape with the same diameter and the same shape for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles with two stages of mating bolt assembly turbines with turbine blades equipped with a heat retaining device driven by heat and accelerated acceleration of liquid metal divided into mass speeds, with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and mass-accelerated are kept in the same diameter and shape of each stage, and are fitted with three bolted assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-split pressure and stored in a mass speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven by mass-accelerated pressure are divided into mass velocities, and the rotor blades of each turbine are of the same shape and shape with the same diameter for each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which turbine blades equipped with a heat retaining device that is driven by mass-acceleration driven with mass-accelerated pressure are divided into mass velocities, and the turbine blades are substantially the same shape for each stage and are fitted in six stages. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycles in which the turbine blades equipped with a heat retaining device that drives the acceleration of the liquid metal by mass acceleration and divided into mass velocities are provided with 7 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in eight stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retaining device with pressure divided and stored at mass speed are substantially the same shape for each stage, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at mass speed are substantially the same shape with the same diameter for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressure divided and stored at mass speed are substantially the same shape for each stage, and a fitting bolt assembly turbine is provided in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行船舶類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Driving various types of flying ships with united engine injection part (78S) injection driving force + Insulating and increasing ball raising device (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is raised and used. Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration + heat retention device with pressures divided and stored at a mass speed are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure that is divided and stored in calorie speed and mass speed + Liquid metal accelerating turbine blades equipped with heat insulation device are made to have the same diameter and shape of each stage in three stages. Various energy conservation cycle coalescence engines provided. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Storage and use + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Turbine blade group equipped with a heat retaining device that accelerates liquid metal by mass Various energy conservation cycle coalescence engine installed in the stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preserving use + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Turbine blades equipped with a heat retention device driven by liquid metal acceleration, with the same diameter and shape of each stage, and fitting bolt assembly turbines in 5 stages Various energy conservation cycle coalescence engine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration by pressure divided and stored in heat quantity speed and mass speed + Liquid metal is heated and heat turbine acceleration turbine blades equipped with heat insulation acceleration, each stage has the same diameter and approximately the same shape, fitting bolt assembly turbine 6 stages Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)で落差増大+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Heat retention increase ball lift device (2F) Increase head drop + Heat retention increase ball lift device (2F) is installed at the corner of the square turbine outer box to raise the liquid metal Preservation + Acceleration with pressure divided and stored in calorie velocity and mass velocity + Seven stages of fitting bolt assembly turbines with turbine blades equipped with a heat retaining device for liquid metal mass acceleration drive with the same diameter and shape of each paragraph Various energy conservation cycle coalescence engine established in. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with turbine blades equipped with a heat retaining device that accelerates with pressure divided and stored in a speed and a heat retaining device for accelerating liquid metal with the same diameter and the same shape for each stage, and 8 stages of fitting bolt assembly turbines . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in the speed are arranged in the same shape with the same diameter and the same shape for each stage, and is provided with 9 fitting bolt assembly turbines. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retention device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with 10 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine blades equipped with a heat retaining device that drives heat acceleration of liquid metal with the same diameter and shape of each stage, and a mating bolt assembly turbine in one stage organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated drive blade group of turbine equipped with heat retaining device, each stage has the same diameter and the same shape, and various energy storage cycles combined with two stages of fitting bolt assembly turbine organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blades equipped with a driving heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with fitting bolt assembly turbines in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in four stages with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and the fitting bolt assembly turbines are provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for acceleration drive are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an acceleration-driven heat retaining device have substantially the same diameter and the same shape for each stage, and are provided with seven fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blade groups equipped with the heat-retaining device for acceleration driving are provided with eight stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates and accelerates by mass are substantially the same shape for each paragraph, and are provided with 9 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerating drive heat retaining device have substantially the same shape and diameter for each stage, and are provided with 10 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which a turbine blade group equipped with a heat-accelerating drive heat insulation device is provided with a fitting bolt assembly turbine in one stage with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescence engines in which turbine blades equipped with a heat retaining device of mass acceleration drive are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device that accelerates the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and three stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the same bolt diameter turbine is provided in five stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and shape of each stage, and 6 bolts of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and approximately the same shape for each paragraph, and with 7 stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with 8 stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines, in which turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates liquid metal with mass are provided with nine stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated by liquid pressure and driven by accelerated pressure are configured to have substantially the same shape and diameter in each stage, and are provided with 10 bolts assembling bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates with accelerated pressure and accelerates the amount of heat of liquid metal are provided in one stage with the same diameter and shape of each turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with two stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines with three stages of fitting bolt assembly turbines with turbine blades equipped with a heat retention device that accelerates with pressure divided and stored, and a heat retaining device for accelerating liquid metal. . タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycles in which turbine blades equipped with a heat retaining device that accelerates and accelerates the liquid metal by mass divided and stored in speed are arranged in four stages with the same diameter and shape of each turbine. Combined organization. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration driven by dividing pressure into speeds are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Combined various energy storage cycles with turbine rotor blades equipped with a heat retention device that drives heat acceleration of liquid metal with the same diameter and the same shape for each stage, and 6 stages of fitting bolt assembly turbines organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+各種飛行機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Drives + Drives various aircrafts into the combined engine injection part (78S) injection driving force + Insulates and increases the temperature of the liquid metal by installing a heat retaining and increasing ball lifting device (2F) at the corner of the rectangular turbine outer box + Heat rate and mass Acceleration with pressure divided and stored at speed + Liquid metal is mass-accelerated and the turbine blades equipped with a heat retaining device are arranged in the same diameter and shape of each stage. organ. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Drives the propulsion force + Insulates and raises the ball riser (2F) at the corner of the square turbine outer box and uses the liquid metal ascending and storing + Accelerates with the pressure divided and stored in the calorie velocity and mass velocity Various energy storage cycle coalescing engines in which turbine blade groups equipped with a driving heat retaining device have substantially the same diameter and the same shape for each paragraph, and are provided with 8 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that is accelerated and driven are arranged in substantially the same shape with the same diameter for each stage, and are provided with 9 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Injection propulsion driving + Insulation sphere raising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate with pressure divided and stored in calorie velocity and mass velocity + Liquid metal acceleration drive Various energy storage cycle coalescing engines in which the turbine blades equipped with the above heat retaining device have substantially the same diameter and the same shape for each stage and are provided with 10 fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating sphere increasing device (2F) is installed at the corner of the square turbine outer box to use the liquid metal ascending and storing + Accelerating with pressure divided and stored in calorie velocity and mass velocity + Heating the liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device are substantially identical in shape with the same diameter for each stage and provided with a fitting bolt assembly turbine in one stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+出力増大球(2E)を重力加速度で下方に加速タービン駆動する+各種航空機類を合体機関噴射部(78S)噴射推進力駆動する+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multi-drive short-time coalescence engine injection unit (78S) Liquid metal solar engine that makes large injection propulsion output + Accelerating sphere (2E) to accelerate turbine by gravity acceleration + Various aircrafts are united engine injection unit (78S) ) Driven by injection propulsion force + Insulating and increasing ball rising device (2F) is installed at the corner of the square turbine outer box to save and use liquid metal + Accelerate by pressure divided and stored in calorie velocity and mass velocity + Mass of liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with an accelerated drive heat retention device have substantially the same shape and diameter in each stage and are provided with two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with the heat-retaining device with acceleration drive are made substantially the same shape with the same diameter for each stage and the fitting bolt assembly turbines are provided in three stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates the mass with a mass are made substantially the same shape with the same diameter for each paragraph and the fitting bolt assembly turbines are provided in four stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blade groups equipped with an acceleration drive heat retention device are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-acceleration-driven heat insulation device are arranged in six stages with fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備駆動して回転方向交互タービンにする+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine to make large injection propulsion output + Horizontal axis (1h) is driven with a square turbine outer box at right angles to drive to rotate direction alternate turbine + Intake air path length Heat and cold production with lens and sunlight + Insulation sphere lifting device (2F) is installed at the corner of the square turbine outer box, and liquid metal is lifted and used for storage + Accelerated with pressure divided and stored in calorie velocity and mass velocity + Liquid metal Various energy storage cycle coalescing engines in which turbine blades equipped with a heat-retaining device for mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The turbine (2F) is installed at the corner of the rectangular turbine outer casing, and the liquid metal is used for ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and the mass velocity + the moving blade of the turbine equipped with the heat retaining device for accelerating the liquid metal Various energy storage cycle coalescing engines, with groups of approximately the same diameter for each paragraph and eight stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise An apparatus (2F) is installed at the corner of the rectangular turbine outer box to use the liquid metal ascending and storing + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the turbine equipped with the heat retaining device that accelerates and drives the liquid metal by mass Various energy storage cycle coalescing engines in which the blade groups are substantially the same shape for each paragraph and the fitting bolt assembly turbines are provided in nine stages. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise Equipment (2F) is installed at the corner of the rectangular turbine outer box, and the liquid metal is used for ascending storage + accelerating with pressure divided and stored in calorie velocity and mass velocity + turbine blades equipped with a heat retention device driven by liquid metal acceleration Various energy storage cycle coalescing engines in which the fitting bolt assembly turbines are provided in 10 stages with the same diameter and the same shape for each paragraph. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the rectangular turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device for the calorie acceleration drive of the liquid metal Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each stage and a single-stage fitting bolt assembly turbine. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにする+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalescence engine injection part (78S) Liquid metal solar thermal engine to make large injection propulsion output + Horizontal axis (1h) has square turbine outer box at right angle to make rotation direction alternate heat insulation turbine + Heat insulation increase sphere rise The equipment (2F) is installed at the corner of the square turbine outer box and the liquid metal is used for ascending storage + accelerating with the pressure that is divided and stored in the calorie velocity and mass velocity + the operation of the turbine equipped with the heat retaining device that drives the liquid metal to mass acceleration Various energy storage cycle coalescing engines with blade groups of the same diameter and the same shape for each paragraph and two stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with the same pressure are provided with three stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量で加速駆動する保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device for accelerating with pressure and accelerating liquid metal with mass are substantially the same shape for each stage, and are provided with four stages of fitting bolt assembly turbines. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device driven by acceleration and liquid metal acceleration at the same pressure are provided with five stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を熱量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which the turbine blades equipped with a heat retaining device that accelerates and accelerates the amount of heat of liquid metal with the same pressure are provided with six stages of fitting bolt assembly turbines with the same diameter and shape of each stage. タービン複数駆動短時間合体機関噴射部(78S)大噴射推進出力にする液体金属太陽熱エンジン+横軸(1h)を角型タービン外箱直角具備して回転方向交互保温タービンにし液体金属を下方に加速駆動する+吸入空気路長レンズと太陽光で温熱冷熱製造+保温増大球上昇装置(2F)を角型タービン外箱角部に設け液体金属を上昇保存使用する+熱量速度と質量速度に分割保存した圧力で加速+液体金属を質量加速駆動の保温装置を具備したタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Turbine multiple drive short-time coalesced engine injection part (78S) Liquid metal solar engine with large injection propulsion output + horizontal axis (1h) is provided with a square turbine outer box at right angles to make the rotating direction alternate heat retaining turbine and accelerate the liquid metal downward Driving + Intake air path length lens and solar heating / cooling production + Insulation sphere raising device (2F) is installed in the corner of the square turbine outer box to save and use liquid metal + Divide and save into heat rate and mass rate Various energy storage cycle coalescing engines in which turbine blades equipped with a heat retaining device that accelerates and accelerates liquid metal with mass acceleration are provided with seven stages of fitting bolt assembly turbines with the same diameter and shape of each stage. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを8段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully automatic machining of turbine blade groups, with the same diameter and shape of each paragraph, and 8 stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを9段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully-automatically machined turbine blade groups, with the same diameter and shape of each paragraph, and with 9 bolted bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを10段に設けた各種エネルギ保存サイクル合体機関。   Various energy conservation cycle coalescing engines with fully-automatically machined turbine blade groups having the same diameter and shape of each paragraph, and 10 fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを1段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully automatic machining turbine blade groups with the same diameter and shape of each paragraph, and a single bolted turbine assembly. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを2段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully-automated turbine rotor blade groups with the same diameter and shape of each paragraph, and two stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを3段に設けた各種エネルギ保存サイクル合体機関。   Various energy conservation cycle coalescing engines with fully-automated turbine rotor blade groups with the same diameter and shape of each paragraph, and three stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを4段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully automatic machining of turbine blades, with the same diameter and shape of each paragraph, and with four stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを5段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully-automatically machined turbine blade groups, each with the same diameter and shape of each stage, and 5 stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを6段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully automatic machining of turbine blade groups, with the same diameter and shape of each paragraph, and with 6 stages of fitting bolt assembly turbines. 全自動加工が可能なタービンの動翼群を段落毎同径略同形として嵌合ボルト組立タービンを7段に設けた各種エネルギ保存サイクル合体機関。   Various energy storage cycle coalescing engines with fully automatic machining of turbine blades that have the same diameter and shape of each stage, and are provided with 7 stages of fitting bolt assembly turbines. タービン翼断面(4A)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 25 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with an injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a double turbine blade cross section (4A) is made into a fitting bolt assembly with the same diameter and shape of each turbine as a stage, and a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with a triple cross section (4A) turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box provided with a quadruple turbine blade cross section (4A). The short-term coalescence engine injection unit that flies with an injection propulsion force to make a fitting bolt assembly with the same diameter and shape of each stage. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 5 times the turbine blade cross section turbine blade group of turbine turbine blades with the same diameter and shape of each paragraph, and the assembly bolt assembly to fly with injection propulsion force for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 6 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with a 7-fold turbine blade cross section turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 8 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with an injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を9倍に設けた2種類のタービン回転出力で駆動する水吸引噴射の噴射推進出力発生方法各種エネルギ保存サイクル合体機関。   Various types of energy storage cycle coalescence engines for generating water jet injection propulsion output driven by two types of turbine rotation output with turbine blade cross section (4A) 9 times larger. タービン翼断面(4A)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) is provided 10 times the turbine blades of the square turbine outer box with the same diameter and approximately the same shape for each stage, and is assembled with a fitting bolt assembly for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with a 11-fold turbine blade cross section, turbine blades of a square turbine outer box having the same diameter and shape of each paragraph, and flying with an injection propulsion force assembling bolt assembly for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with a 12-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage, flying with an injection propulsion force, and a short-time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box with a turbine blade cross-section (4A) 13 times larger. The short-term coalesced engine injection unit that flies with an injection propulsion force that forms a fitting bolt assembly with the same diameter and shape of each stage. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross-section (4A) 14 times as large as the same diameter and approximately the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with 15 times the turbine blade cross section (4A) turbine blades of the turbines with the same diameter and the same shape for each paragraph and flying with the injection propulsion force assembling bolt assembly for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with 16 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph, and flying with injection propulsive force to assemble with bolts for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 17 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 18 times the turbine blade cross-section turbine blade group of turbines with the same diameter and shape of each paragraph, and flying with injection propulsion force assembling bolt assembly for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with a 19-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage and flying with an injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 20 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with injection propulsion force to assemble with a short time united engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4A) 21 times larger, and a short-term coalescence engine injection unit that flies with an injection propulsion force assembling bolts with the same diameter and shape of each stage. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 22 times the turbine blade cross section turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with injection propulsion force for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) with 23 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each stage and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4A)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4A) provided with 24 times the turbine blade cross section turbine blade group of turbine turbine blades with the same diameter and shape of each stage, flying with injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   The turbine blade section of the square turbine outer box with a turbine blade cross-section (4B) 25 times larger is made into a fitting bolt assembly with the same diameter and the same shape for each paragraph, and the united engine injection section for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a double turbine blade cross-section (4B), with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box provided with triple turbine blade cross section (4B) is made into a fitting bolt assembly with the same diameter and shape of each turbine as a stage, and then a unitary engine injection unit for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with quadruple turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box provided with a turbine blade cross section (4B) five times as long as it is flying with injection propulsion force to make a fitting bolt assembly with the same diameter and shape of each paragraph for a short time united engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   The turbine blade section of the square turbine outer box provided with 6 times the turbine blade cross section (4B) has the same diameter and the same shape for each paragraph and is assembled with a fitting bolt assembling for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with a turbine blade cross section (4B) of 7 times the turbine blades of the turbine of the same type with the same diameter and the same shape for each paragraph and flying with the injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 8 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and approximately the same shape for each paragraph and flying with injection propulsive force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を9倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with a nine-fold turbine blade cross section, turbine blades in a square turbine outer box having the same diameter and shape of each stage, and flying with an injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with a 10-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage, and flying with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with 11 times the turbine blade cross section (4B) turbine blade group of turbines with the same diameter and approximately the same shape for each paragraph and flying with the injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 12 times the turbine blade cross-section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 13 times the turbine blade cross-section turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with injection propulsion force for short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 14 times the turbine blade cross-section turbine blade group of turbines with the same diameter and shape of each stage, and flying with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with 15 times the turbine blade cross section (4B) The turbine blades of the turbine blade box with the same diameter and the same shape for each paragraph and flying with the injection propulsion force assembling bolt assembly for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with 16 times the turbine blade cross section, turbine blades of a square turbine outer box with the same diameter and shape of each stage as a fitting bolt assembly and flying with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with 17 times the turbine blade cross section (4B), the turbine blades of the turbine are boxed in the same diameter and in the same shape for each stage, and are assembled with a fitting bolt assembly to fly for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) with 18 times the turbine blade cross section (4B) turbine blades in the same diameter and shape of each stage as a fitting bolt assembly to fly by injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 19 times the turbine blade cross section turbine blade group of turbine turbine blades with the same diameter and shape of each stage, and a combination bolt assembly to fly with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with 20 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with the injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4B) 21 times as large as the same diameter and shape of each stage as a fitting bolt assembly. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross section (4B) 22 times larger, with the same diameter and approximately the same shape for each paragraph, flying with an injection propulsion force to make a short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) provided with a turbine blade cross-section (4B) of 23 times the turbine blades in the same diameter and shape of each stage as a fitting bolt assembly and flying for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4B)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4B) is provided 24 times larger than the turbine blades of the square turbine outer box with the same diameter and the same shape for each paragraph, and the assembly bolt is assembled for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 25 times the turbine blade cross section turbine blade group of turbine turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a doubled turbine blade cross-section (4C), flying with injection propulsion force to make a fitting bolt assembly with the same diameter and shape of each paragraph, and a short-time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section in a square turbine outer box with three times the turbine blade cross section (4C), and the turbine blades in the same diameter and the same shape for each paragraph and flying with the injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box provided with a quadruple turbine blade cross section (4C), and flying with an injection propulsion force to make a fitting bolt assembly with the same diameter and the same shape for each paragraph. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with a five-fold turbine blade cross section, turbine blades of a square turbine outer box having the same diameter and shape of each paragraph, and flying with an injection propulsion force assembling bolt assembly for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 6 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a turbine blade cross section (4C) 7 times larger, with the same diameter and the same shape for each paragraph and flying with an injection propulsion force assembling bolt assembly for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box provided with a turbine blade cross section (4C) 8 times larger, with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を9倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box with a turbine blade cross-section (4C) 9 times as large as the same diameter and shape of each stage as a fitting bolt assembly. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with 10 times the turbine blade cross section turbine blade group of turbine turbine blades with the same diameter and shape of each stage, and a combination bolt assembly to fly with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box having a turbine blade cross section (4C) 11 times as large as the same diameter and the same shape for each paragraph and flying with an injection propulsion force to make a short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with 12 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with an injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 13 times the turbine blade cross section turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with a 14 times larger turbine blade cross section (4C) turbine blades in the same diameter and shape of each stage of the turbine, and fly with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box with a turbine blade cross section (4C) provided 15 times larger than the same diameter and the same shape for each paragraph and flying with an injection propulsion force assembling bolt assembly for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with 16 times the turbine blade cross section turbine blade group turbine blades of the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 17 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section in a square turbine outer box with a turbine blade cross section (4C) 18 times larger, with the same diameter and approximately the same shape for each paragraph, flying with an injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 19 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph, and flying with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with a 20 times larger turbine blade cross section turbine blade group of turbine blades having the same diameter and shape of each stage, and flying with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with a turbine blade cross section (4C) 21 times larger, turbine rotor blade group with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4C) 22 times larger, with the same diameter and the same shape for each paragraph as a fitting bolt assembly, and flying with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) provided with 23 times the turbine blade cross section, turbine blades of the square turbine outer box with the same diameter and shape of each stage as a mating bolt assembly and flying for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4C)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4C) with 24 times the turbine blade cross-section turbine blade group of turbine turbine blades with the same diameter and shape of each stage, flying with injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 25-fold turbine blade cross section turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with double turbine blade cross-section (4D), with the same diameter and approximately the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a triple cross section (4D) The turbine blades of the turbine box with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) provided with quadruple turbine blades in the turbine casing of the turbine of the turbine type, with the same diameter and approximately the same shape for each paragraph and flying with injection propulsive force for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a five-fold turbine blade cross section, turbine blades of the same type with the same diameter and shape of each stage as a fitting bolt assembly. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 6-fold turbine blade cross section, the turbine blades of the turbine are boxed in the same diameter and in the same shape for each stage, and are assembled with a fitting bolt assembly for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 7-fold turbine blade cross section, turbine blades of the turbine turbine box with the same diameter and shape of each paragraph, and flying with injection propulsion force assembling bolt assembly for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) is provided with 8 times the turbine blade section of the turbine of the square-shaped turbine outer casing, and the unit is a short time coalescence engine injection unit flying with the injection propulsion force assembling bolt assembly with the same diameter and shape of each paragraph (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を9倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a nine-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each stage and flying with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) 10 times larger than the turbine blades of the square turbine outer box, each stage has the same diameter and approximately the same shape and fly with injection propulsion force to assemble the bolts for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 11 times larger cross section (4D) turbine blades of turbine blades with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross-section (4D) 12 times larger, with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 13 times larger cross section (4D) turbine blade group turbine blades with the same diameter and the same shape for each stage and flying with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) is provided 14 times the turbine blades of a square turbine outer box with the same diameter and the same shape for each stage, and is assembled with a fitting bolt assembly for short-time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 15 times larger cross section (4D) turbine blade group turbine blades with the same diameter and the same shape for each stage and flying with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 16 times larger cross section (4D) turbine blades of turbine blades with the same diameter and the same shape for each stage, and a combination bolt assembling to fly with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 17 times larger cross section (4D) turbine blade group of turbine blades with the same diameter and shape of each stage, and a combination bolt assembling to fly with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 18-fold turbine blade cross section, turbine blades in a square turbine box with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) provided with 19 times the turbine blade section of the turbine of the square-shaped turbine outer casing and flying with the injection propulsion force to make the assembly bolt assembly with the same diameter and the same shape for each paragraph (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) with a 20 times larger cross section (4D) turbine blades of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section in a square turbine outer box with a turbine blade cross-section (4D) 21 times larger, with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) provided with 22 times the turbine blade cross section turbine blade group of the same diameter and shape of each stage as a fitting bolt assembly to fly with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross-section (4D) of 23 times the same diameter and shape of each stage as a fitting bolt assembly and flying with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4D)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4D) provided 24 times larger than the turbine blades of the square turbine outer box with the same diameter and the same shape for each paragraph and flying with the injection propulsion force for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 25 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage, and a combination bolt assembly to fly with a jet propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a double turbine blade cross-section (4E), and a short-term coalescence engine injection unit flying with injection propulsion force assembling bolt assembly with the same diameter and shape as each paragraph (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a triple turbine blade cross-section (4E). The turbine blades of the turbines have the same diameter and the same shape for each stage. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a quadruple turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage, and a combination bolt assembly to fly with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a five-fold turbine blade cross section, turbine blades of the same type with the same diameter and shape of each stage as a fitting bolt assembly. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with 6 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage and flying with injection propulsion force to assemble with bolts for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a 7-fold turbine blade cross section, turbine blades of the turbine box of the same type with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 8 times the turbine blade cross section (4E) turbine rotor blade group with the same diameter and shape of each stage as a mating bolt assembly and flying for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を9倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 9 times the turbine blade cross-section turbine blades of the same size and shape of each stage of the turbine blades and flying with injection propulsion force to assemble the bolts for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with 10 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 11 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph, and flying with injection propulsion force to assemble with bolts for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with 12 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with 13 times the turbine blade cross section (4E) turbine blades of the turbine turbine box with the same diameter and the same shape for each paragraph and flying with injection propulsion force for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) is provided 14 times the turbine blades of the square-type turbine outer box with the same diameter and approximately the same shape for each stage, and is assembled with a fitting bolt for short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a 15-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each stage, flying with injection propulsion force to assemble with bolts for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) is provided 16 times the turbine blades of the square turbine outer box with the same diameter and the same shape for each stage, and the assembly bolt is assembled for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   The turbine blade section of a square turbine outer box having a turbine blade cross-section (4E) 17 times larger is made into a fitting bolt assembly with the same diameter and the same shape for each paragraph, and is short-term combined engine injection section (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 18 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph and flying with the injection propulsion force to make a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a 19-fold turbine blade cross section turbine blade group of turbine blades having the same diameter and shape of each stage, and flying with an injection propulsion force assembling bolt assembly for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) with a 20-fold turbine blade cross section turbine blade group of turbine blades with the same diameter and shape of each paragraph, and a combination bolt assembly to fly with injection propulsion force for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with a turbine blade cross section (4E) 21 times larger. The turbine blades of the turbine are of the same diameter and the same shape for each stage. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 22 times the turbine blade cross section turbine blade group of the same diameter and shape of each stage as a fitting bolt assembly to fly by injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 23 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4E)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4E) provided with 24 times the turbine blade cross section (4E) turbine blades in the same diameter and shape of each stage as a fitting bolt assembly to fly by injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を25倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) provided with 25 times the turbine blade cross section turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を2倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box with a doubled turbine blade cross section (4F) with the same diameter and the same shape for each paragraph as a fitting bolt assembly and flying with a jet driving force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を3倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   The turbine blade section of a square turbine outer box having a turbine blade cross section (4F) tripled is made into a fitting bolt assembly with the same diameter and the same shape for each paragraph, and the unit is injected for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を4倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   A short time coalescence engine injection unit that flies with the injection propulsion force that makes the moving blade group of the turbine of the square turbine outer casing provided with quadruple turbine blade cross section (4F) the same diameter and approximately the same shape for each paragraph. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を5倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box having a turbine blade cross section (4F) 5 times larger, and a short-term coalescence engine injection unit flying with injection propulsion force assembling bolt assembly with the same diameter and shape of each paragraph (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を6倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross section (4F) 6 times larger, with the same diameter and the same shape for each paragraph and flying with an injection propulsion force assembling bolt assembly for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を7倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box having a turbine blade cross section (4F) seven times as large as the same diameter and shape of each stage as a fitting bolt assembly. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を8倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-shaped turbine outer box having a turbine blade cross section (4F) 8 times larger, with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を9倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with a nine-fold turbine blade cross-section turbine blade group of turbines with the same diameter and shape of each stage, and a combination bolt assembling to fly with injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を10倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with 10 times the turbine blade cross section (4F) turbine blade group of turbine blades with the same diameter and the same shape for each paragraph and flying with injection propulsion force for a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を11倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box with 11 times the turbine blade cross section (4F) is made into a fitting bolt assembly with the same diameter and shape of each stage as a stage, and a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を12倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4F) 12 times larger, with the same diameter and the same shape for each paragraph as a fitting bolt assembly, and flying with injection propulsion force for a short time combined engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を13倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box having a turbine blade cross section (4F) of 13 times the same diameter and shape of each stage as a fitting bolt assembly and flying with an injection driving force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を14倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square-type turbine outer box having a turbine blade cross-section (4F) 14 times larger, with the same diameter and approximately the same shape for each paragraph, and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を15倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with 15 times the turbine blade cross section (4F) The turbine blades of the turbine are boxed in the same diameter and in the same shape for each stage, and are assembled with a fitting bolt assembly for a short time. (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を16倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with 16 times the turbine blade cross section (4F) turbine blades in the same diameter and approximately the same shape for each paragraph and flying with the injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を17倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with a 17 times larger turbine blade cross section (4F) turbine blades of the same diameter and shape of each stage as a fitting bolt assembly for short-term combined engine injection (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を18倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with 18 times the turbine blade cross-section (4F) turbine blades of the same size and shape of each stage of the turbine, and fly with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を19倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) provided with 19 times the turbine blade cross section turbine blade group of the same diameter and shape of each stage as a fitting bolt assembly to fly by injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を20倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with a 20 times larger turbine blade cross section (4F) turbine blades in the same diameter and shape of each stage, and flying with injection propulsion force to assemble the bolts for a short time (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を21倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4F) 21 times larger, and a short-term coalescence engine injection section flying with injection propulsion force to make assembly bolt assembly with the same diameter and shape of each paragraph (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を22倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade section of a square turbine outer box having a turbine blade cross section (4F) 22 times larger, with the same diameter and approximately the same shape for each paragraph, flying with an injection propulsion force to make a short-term coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を23倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with a turbine cross section (4F) of 23 times the turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with an injection propulsion force for a short time coalescence engine injection unit (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. タービン翼断面(4F)を24倍に設けた角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする噴射推進力で飛行して短時間合体機関噴射部(78S)大量噴射して宇宙に到達飛行する各種エネルギ保存サイクル合体機関。   Turbine blade cross section (4F) with 24 times the turbine blade cross section (4F) turbine blade group of turbines with the same diameter and the same shape for each paragraph and flying with injection propulsion force to make a short time coalescence engine injection part (78S) Various energy conservation cycle coalescing engines that fly in large quantities and fly to space. 角型タービン外箱のタービンの動翼群を段落毎同径略同形として嵌合ボルト組立にする駆動熱ポンプで太陽光加熱した空気を吸入圧縮高温とし、圧縮熱回収器(2C)で熱回収して燃料噴射燃焼熱交換冷却燃焼して、燃焼ガス熱量と質量に分割保存して短時間合体機関噴射部(78S)大熱量噴射して宇宙飛行にする飛行機類とした各種エネルギ保存サイクル合体機関。   The turbine blades of the square turbine outer box have the same diameter and the same shape for each paragraph, and are assembled with fitting bolts. The air heated by sunlight with the drive heat pump is made into the intake compression high temperature, and the heat is recovered with the compression heat recovery unit (2C). Fuel-injection-combustion-heat-exchange-cooling-combustion-divided and stored into combustion gas heat quantity and mass, and short-time coalescence engine injection part (78S) .
JP2009101707A 2009-03-03 2009-04-20 Combination engine with various energy conservation cycle Pending JP2010255418A (en)

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