JP2011169117A - Various energy conservation cycle combined engine - Google Patents
Various energy conservation cycle combined engine Download PDFInfo
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- JP2011169117A JP2011169117A JP2009279964A JP2009279964A JP2011169117A JP 2011169117 A JP2011169117 A JP 2011169117A JP 2009279964 A JP2009279964 A JP 2009279964A JP 2009279964 A JP2009279964 A JP 2009279964A JP 2011169117 A JP2011169117 A JP 2011169117A
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
- Y02E10/46—Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines
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本発明はスクラムジェットの高速燃焼と蒸気タービンの高圧大膨張速度とロケットを合体し、宇宙で無限大容積の過熱蒸気を500度等に加熱噴射して膨張速度を更に増大する、合体機関噴射部78W太陽熱重力ヘリコプター39Cとし、又熱ポンプで使用電力の3〜10倍の熱エネルギが得られる情報があり、太陽熱を種に大気圧同速度同容積仕事率最高が、既存蒸気タービンの3.6万倍白金球仕事率重力タービン駆動熱ポンプで圧縮熱回収して、3〜10倍の温熱と冷熱両方のエネルギを無限回収利用のエネルギ保存サイクルにし、太陽光加熱の空気を吸入圧縮1000度等として、太陽光加熱別空気を加熱吸入圧縮1200度等とし、熱交換過熱蒸気50+圧縮空気28aを製造する操作を複数回実施して、理論最良の推進剤過熱蒸気50+酸化剤圧縮空気28a無限製造に燃料費0でも挑戦し、合体機関噴射部78W噴射は、燃焼器1Yに圧縮空気供給燃料噴射燃焼1200度等として、外周過熱蒸気50を加熱最高温度燃焼にし、噴射の過程で過熱蒸気50の外周に設けた、複数の燃焼ガス噴射ノズル6Y高温高速燃焼内に燃料噴射2段燃焼して、過熱蒸気50の外周を1200度に近付けて、0〜100度に近付く過熱蒸気を800度等に加熱し、過熱蒸気容積を増大して、噴射推進出力と燃焼ガス49の吸引出力を真空で最大にし、燃焼ガス吸引出力の増大によりスクラムジェットの欠点を解消して、最大3.6万倍仕事率回転翼駆動を含めて空気抵抗0CO2排気0の宇宙利用全盛を狙う、合体機関噴射部78W太陽熱重力ヘリコプター39C等の技術に関する。 The present invention combines a rocket with high-speed high-speed combustion of a scramjet and high-pressure high-expansion velocity of a steam turbine, and heats and injects superheated steam of infinite large volume in space etc. in space to further increase the expansion velocity. 78 W solar thermal gravity helicopter 39C, and there is information that thermal energy can be obtained 3 to 10 times the power used by a heat pump, solar pressure is the same as atmospheric pressure same velocity work volume highest rate is 3.6 of the existing steam turbine 10,000 times platinum sphere work rate Gravity turbine driven heat pump to recover compression heat, 3 to 10 times energy of both heat and cold heat to infinite recovery utilization energy preservation cycle, air of solar heating is suctioned compression 1000 degree etc As solar heating air separate heating and suction compression 1200 degrees etc., the heat exchange superheated steam 50 + compressed air 28a is performed several times to carry out the operation several times, theoretically the best propellant superheated steaming Challenge the 50+ oxidant compressed air 28a infinite production even at fuel cost 0, united engine injection part 78W injection makes the peripheral superheated steam 50 the maximum temperature combustion, with compressed air supply fuel injection combustion 1200 degree etc. to the combustor 1Y, In the process of injection, a plurality of combustion gas injection nozzles 6Y provided on the outer periphery of the superheated steam 50 burn fuel in two stages during high temperature high speed combustion, and bring the outer periphery of the superheated steam 50 close to 1200 degrees By heating the approaching superheated steam to 800 degrees etc., increasing the superheated steam volume, maximizing the injection propulsion output and the suction output of the combustion gas 49 with vacuum, and eliminating the defect of the scramjet by increasing the combustion gas suction output Regarding technology such as combined engine injection unit 78 W solar thermal gravity helicopter 39C aiming at space utilization of air resistance 0 CO 2 exhaust 0 including maximum 36,000 times power ratio rotary wing drive
燃料費僅少の太陽熱重力ヘリコプター39C等で燃料費0の宇宙利用全盛を狙うもので、大気中では太陽光で加熱した空気を、竪型被覆金属球重力太陽熱衝撃低減タービン駆動熱ポンプ1Gで吸入圧縮熱交換熱回収して、必要に応じて圧縮熱交換熱回収複数回の過程で燃料噴射燃焼熱交換過熱蒸気50を製造し、酸化剤の圧縮空気28a冷熱乃至燃焼ガス49冷熱と推進剤の過熱蒸気50を製造して、宇宙では被覆金属球の圧縮空気加速タービン駆動で低圧低温とした熱回収循環とし、直射太陽光120度Cと長レンズ2dと熱ポンプにより過熱蒸気製造効率を上昇して、宇宙上昇時は圧縮空気28a圧縮熱回収器2Cで過熱蒸気50製造の過程で、複数回燃料噴射燃焼燃焼ガス49にして、24〜400MPa過熱蒸気製造量を増大し、合体機関噴射部78W燃焼器1Yに燃焼ガスを供給その外周に過熱蒸気を供給して、24〜400MPa燃焼ガス49に燃料噴射燃焼外周の過熱蒸気を加熱し、2段燃焼や3段燃焼以後は過熱蒸気を内週と外周から最適時間環状加熱して、更に大幅な噴射推進出力の増大を可能に、空気28a吸入路最適位置に複数の燃料噴射ノズル6Xを具備し、燃料噴射着火燃焼して短時間大幅な燃料燃焼量の増大と噴射推進出力の増大として、蒸気タービンの高圧大膨張速度とスクラムジェットの高速燃焼とロケットを合体し、既存ジェット機の10〜100倍圧力10倍熱量噴射100〜1000倍噴射出力狙い、実験最良エンジンに移行の合体機関噴射部78W技術に関する。 Aim for zero fuel cost space use with solar thermal gravity helicopter 39C etc. with minimal fuel cost. Air heated by solar light in the atmosphere, suction and compression with vertical coated metal sphere gravity solar thermal shock reduction turbine driven heat pump 1G Heat exchange heat recovery and, if necessary, compression heat exchange heat recovery Multiple-shot fuel injection combustion heat exchange superheated steam 50 is produced, compressed air 28a of the oxidant cold air to combustion gas 49 cold of the combustion gas and superheat of the propellant The steam 50 is produced, and in the space, the heat recovery circulation is made low pressure low temperature by compressed air acceleration turbine drive of coated metal balls, and the superheated steam production efficiency is raised by direct sunlight 120 degrees C, long lens 2d and heat pump In the process of producing superheated steam 50 with compressed air 28a compression heat recovery device 2C, when the space climbs, increase the amount of 24-400MPa superheated steam production by combining it with fuel injection combustion combustion gas 49 multiple times, Supply the combustion gas to the outer periphery of the engine injection unit 78W combustor 1Y and supply the overheated steam to the outer periphery, heat the overheated steam of the fuel injection combustion outer periphery to the 24-400MPa combustion gas 49, and overheat after the two-stage combustion or the three-stage combustion Annular heating of the steam from the inner week and outer circumference for optimum time, further increasing the injection propulsion power, equipped with multiple fuel injection nozzles 6X at the optimum position of the air 28a suction path, fuel injection ignition combustion and short The rocket is combined with the high pressure large expansion speed of the steam turbine and the high speed combustion of the scramjet as the increase of the fuel combustion amount and the injection propulsion power increase for a long time, 10 to 100 times the pressure 10 times the thermal energy injection 100 to 1000 of the existing jet. It is related to the combined engine injection part 78 W technology that aims at double injection output and shifts to the experimental best engine.
竪型被覆金属球重力衝撃低減温熱タービン8G+竪型被覆金属球重力衝撃低減冷熱タービン8Gとして、水銀や液体金属(鉛合金中核500度以下液体金属合金)を衝撃低減材料3Eとし、金属球を(合金を含む白金球・金球・タングステン球・鋼球・モリブデン球・鋳鉄球・銀球・銅球・ニッケル球・コバルト球・クロム球)等として、被覆金属球を金属球に被覆を設けたものとし、液体金属を500度以下で液体の金属として、液体金属の中核を鉛合金とし、資源量に最適対応した温熱タービン+冷熱タービン駆動として、被覆金属球を金属噴射ポンプ6M等で噴射し、温熱加速+冷熱加速でタービン駆動重力中核加速して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にしたタービン翼8cに噴射し、被覆金属球の転がり接触回転出力の増大として、竪型被覆金属球重力衝撃低減タービン8G回転にし、長レンズ2d熱吸収材2Bで構成の吸入空気路28A太陽熱加熱の空気28aを吸入して、熱ポンプで圧縮900度前後にし、圧縮熱回収器2Cで熱交換太陽熱加熱の空気28aを500度前後に加熱して、吸入圧縮1200度等にし、熱回収を継続して圧縮空気28a温熱冷熱製造を無限継続膨大として、大気圧同速度同容積仕事率kg重m/秒最高を、既存蒸気タービンの3.6万倍白金球仕事率前後にし、実験最良に移行の竪型被覆金属球重力衝撃低減タービン8G技術に関する。 Vertical-shaped coated metal ball Gravity impact reduction thermal turbine 8G + vertical-type coated metal ball gravity impact reduction cold heat turbine 8G, mercury or liquid metal (lead alloy core 500 degrees or less liquid metal alloy) as impact reduction material 3E, metal balls ( Coated metal spheres were coated on metal spheres, such as platinum spheres, gold spheres, tungsten spheres, steel spheres, molybdenum spheres, cast iron spheres, silver spheres, copper spheres, nickel spheres, cobalt spheres, chromium spheres, etc. Liquid metal is used as a liquid metal at a temperature of 500 degrees or less, the core of liquid metal is a lead alloy, and a coated metal ball is injected by a metal injection pump 6M etc. as a thermal turbine + cold thermal turbine drive that optimally corresponds to the amount of resources. Thermal acceleration + thermal acceleration accelerates the turbine driven gravity core and injects the turbine blade cross section 4X into the turbine blade 8c which is 2 to 26 times larger than the existing steam turbine, and the rolling contact of the coated metal ball In order to increase the displacement output, the vertical coated metal ball gravity shock reduction turbine 8G is rotated, and the intake air passage 28A constituted by the long lens 2d heat absorbing material 2B is drawn in and the air 28a of solar thermal heating is compressed by a heat pump around 900 degrees. The heat exchange solar heating air 28a is heated to around 500 degrees in the compression heat recovery unit 2C to make the suction compression 1200 degrees etc., and the heat recovery is continued to make the compressed air 28a thermal cold and cold heat production infinite and huge. The air pressure isospeed same volumetric work rate kg heavy m / s maximum is about 36,000 times platinum ball work rate of the existing steam turbine, and it is experiment best about vertical type coated metal sphere gravity impact reduction turbine 8G technology of transition.
3.6万倍白金球仕事率理論最良タービン等から現状を人類絶滅の陰謀と考えると、火力原子力発電の海面温度7度上昇は環境に影響皆無としておりますが、海面温度が周囲より7度上昇すると蒸発量が爆発的に増大し、異常気象発生は明白で周囲の海水と混合分散すると海面全部が温度上昇するため、冬場に海面冷却海底に窒素や酸素やCO2等の栄養分を供給していた自然現象を不可能にして、魚類や海草類等人類の食糧が激減するため現状と一致し、海面温度7度上昇を100年続け、原子力発電でCO2排出量を低減しても、海水表面温度7度上昇海域が10%成長で1000倍を超えるため、海水中のCO2を大気中に放出CO2濃度を大幅増大して、旱魃や豪雨や風速を10倍の300m/秒台風や季節風として南極の氷を0に近付け、陸と海の食糧が0に近付き、人類が絶滅に近付く背景があります。IPCC北極予測も海面温度7度上昇がコンピュータ計算外のため、衛星07年観測北極海海氷面積がIPCC第4次報告書の40年後に近い状態で観測された報道があり、IPCC予測全部を大誤報と考えるのが良く、平均的に1度温度上昇しても異状気象は困難で、90%前後が海面温度7度上昇と考えると、100年前後で海面温度7度上昇を2〜3回上昇14〜21度上昇海域が南極に接近し、南極の氷が0に近付き、海面上昇が77mに近付く背景があります。 Considering that the present situation is a conspiracy of human extinction from the 360,000 times platinum sphere work rate theory best turbine etc., the sea surface temperature rise of thermal power nuclear power is considered to have no effect on the environment, but the sea surface temperature is 7 degrees from the surrounding The amount of evaporation explosively increases when rising, abnormal weather occurrence is obvious, the whole surface rises when mixed and dispersed with the surrounding sea water, so nutrients such as nitrogen, oxygen and CO2 are supplied to the surface-cooled seabed in winter It is consistent with the present situation as the natural phenomena become impossible and the food of human beings such as fish and seaweeds decreases sharply, and the sea surface temperature rises 7 degrees continuously for 100 years, and even if CO2 emissions are reduced by nuclear power generation, the sea surface temperature As the 7 ° Climb region is 10% growth and exceeds 1000 times, CO2 in seawater is released into the atmosphere, and the concentration of CO2 is significantly increased, resulting in dredging, heavy rainfall, 10 times the wind speed, 300 m / s, typhoon Ice to 0 Put, close to the land and the sea food is 0, there is a background that humanity is close to extinction. Also, there is a report that the satellite's observation of the 2007 Arctic Ocean ice area is observed 40 years after the IPCC Fourth Report, because the IPCC Arctic forecast also has a 7-degree sea surface temperature rise outside the computer calculation. It is good to think that it is a big false alarm, abnormal weather is difficult even if the temperature rises by 1 degree on average, and assuming that 90% rise in the sea surface temperature by 7 degrees, rise in the sea surface temperature by 7 degrees around 100 years by 2-3 Rising 14-21 degrees Rise area approaches to Antarctica, ice on Antarctica approaches 0, there is a background that sea level rise approaches 77m.
高校や大学で既存エンジンを理論最良エンジンと説明しており、小学校理科に戻って理論最良エンジンを考えると、仕事率の単位がkg重m/秒等重量×速度のため、重い物質を高速度にして回転出力発生が理論最良エンジンですが考えた痕跡が皆無という背景があります。そこで消費燃料僅少の竪型被覆金属球重力衝撃低減タービン8G駆動飛行機類や船舶類にして、停止中は熱と電気と冷熱の供給設備で使用可能に地球温暖化防止する等とし、大気圧同速度同容積仕事率kg重m/秒最高を既存蒸気タービンの3.6万倍前後白金球仕事率にして、水銀・液体鉛・液体錫・液体亜鉛等液体金属や金属球や被覆金属球を垂直下方に重力加速度加速にすると、低速で落差を増大する入力より重力加速度加速だけでも出力発生は大幅に増大し、タービンの大型化多数化+落差を1000m以上に増大限り無く出力を増大できる背景があります。地球での最大加速が重力加速度で無限大に近く、海水温度上昇0やCO2排気0や燃料費0の理論最良エンジン重力太陽熱発電として、化石燃料等限りある資源が枯渇するため、限りある資源を子孫に残す手段の温熱や冷熱の回収利用無限大や無限大に近い発電量とし、重力太陽熱発電蓄電池駆動や電気駆動の、各種自動車類全盛や各種船舶類全盛や全面電化住宅全盛や工場電化全盛等、極端に安価な発電の蓄電池駆動や電気駆動の地球温暖化防止が得られる背景があります。 High school or university describes the existing engine as the theoretical best engine, and returns to elementary school science and thinks about the theoretical best engine, the unit of work rate is kg weight m / s equal weight x speed, so heavy material with high speed The rotational power generation is the theoretical best engine, but there is a background that there is no trace considered. Therefore, it is considered that the consumption of fuel will be limited to a cage-type coated metal ball gravity impact reduction turbine 8G drive airplanes and ships, etc., while stopping the use of heat, electricity and cold heat supply equipment to prevent global warming etc. Speed and volume work load kg weight m / s The maximum is about 36,000 times the platinum steam work rate of the existing steam turbine, and the liquid metal such as mercury, liquid lead, liquid tin, liquid zinc, metal spheres and coated metal spheres If gravity acceleration is applied vertically downward, output generation will be greatly increased by gravity acceleration acceleration only from input that increases the drop at low speed, and the number of turbines can be increased and the drop can be increased to 1000 m or more. there is. The maximum acceleration on the earth is close to infinity by the gravitational acceleration, and the theoretical best engine gravity solar power of sea water temperature rise 0, CO2 exhaust 0 and fuel cost 0 is exhausted, as limited resources such as fossil fuel are exhausted. Thermal energy and cold energy recovery means to leave to descendants Infinite or almost infinite power generation, Gravity solar thermal power storage battery driven and electric driven, various kinds of cars and ships, various kinds of ships, and full electrification houses and factories electrification Such as, there is a background that can be obtained storage battery drive of extremely cheap power generation and prevention of global warming of the electric drive.
外れて欲しい予想は、中国が10%成長を50年続けると海水温度上昇量が現在の32倍になり、日本の季節風が50〜80m/秒となって国土全部が海水に汚染され、農業と緑が壊滅して餓死者続出が類似世界に拡大する可能性があり、今の雇用不安も小泉総理に再三予想を提供の日本大企業80%前後ゴーストタウン化が始まったのではと心配、危機をチャンスにする知恵が必要です。昭和17〜18年に理論最良エンジンの発明を決意実際は改良から始め、昭和38年岡山地方発明センターの請負で試作を開始して、自分でも試作を続けましたがエンジンの試作は非常に困難です。そこで昭和57年2月より国内大企業等多数にご協力のお願い始めましたが、日本企業等の協力が皆無で、外国唯一お願いしたクリントン大統領の協力がお願いの都度3年3回得られ、1992年米国特許5133305号、1993年米国特許5230307号、1995年米国特許5429078号の駄目発明が判明したのです。既存のエンジンに致命的な欠点が非常に多く改良発明不可能が判明し、急がば回れと1997年ホームページを開設して欠点を1つ改良特許出願して、2008年理論最良エンジンに到達し、元大統領の協力により例えば重力太陽熱発電により燃料費0で発電機及び熱ポンプを駆動して、無限大に近い電気及び温熱と冷熱を極端に安価製造タービン駆動可能とし、500°C以下液体金属発電で、大気圧同速度同容積仕事率を既存蒸気タービン発電の1〜2.3万倍にして、実際に実験して実験最良エンジンに移行したいのです。 It is expected that if China continues to grow at 10% for 50 years, the temperature rise of seawater will be 32 times that of the present, and Japanese monsoon wind will be 50 to 80m / sec, and the whole country will be polluted with seawater. It is feared that the greening of around 80% of Japan's large companies that offer the resumption of the current employment fear to Prime Minister Koizumi may have begun to be around around 80%, as greenery may be destroyed and successive deaths may extend to similar worlds We need wisdom to make Decided to invent the theoretical best engine in 1965. In fact, it began to improve and started trial production at the contract of the Okayama regional invention center in 1955, and continued trial production on its own, but trial production of the engine is very difficult. . Therefore, we started asking for a large number of large domestic companies to cooperate from February 1982. However, there is no cooperation from Japanese companies, etc. The cooperation of President Clinton who only asked foreign countries is obtained three or three times every request. The useless inventions of 1992 US Patent 5133305, 1993 US Patent 5230307 and 1995 US Patent 5429078 have been found. There are many fatal defects in the existing engine, and it turns out that it is impossible to improve the invention, and in a hurry and opens the 1997 home page, one defect patent application is filed and the 2008 theoretical best engine is reached To drive the generator and heat pump at a fuel cost of 0, for example, by gravity solar thermal power generation with the cooperation of the former president, and to enable extremely inexpensive manufacturing turbine drive for near infinite electricity and heat and cold, liquid metal below 500 ° C In power generation, I would like to make an atmospheric pressure same speed same volume work factor 1 to 23,000 times that of existing steam turbine power generation, actually experiment and shift to an experimental best engine.
既存世界の火力原子力発電所では、CO2増大地球温暖化加速や海水表面温度摂氏7度上昇海域を100年で1000倍等とし、大気中のCO2増大地球温暖化加速や海水温度上昇により下降気流や上昇気流を増大して、異常乾燥山火事や旱魃や集中豪雨等を限り無く増大人類の陸上食物を限り無く減少し、冬場に海面冷却海底に栄養分を供給していた自然現象を不可能として、植物プランクトンや海草類やサンゴ等を激減、食物連鎖により魚類を1/100等に激減人類の海中食物も限り無く減少し、旱魃や集中豪雨や台風や季節風を100年で10倍等に増大して、例えば台風や季節風を300m/秒等とし、人類絶滅の危険を増大のため、地球温暖化防止して人類絶滅を先送りする課題が在り、化石燃料を大量に燃焼すると地球が温暖化すると共に資源が枯渇するため、空気抵抗0CO2排気0の宇宙利用全盛の飛行機類にして化石燃料燃焼は必要最少にして、限りある資源を子孫に残すと共に海水温度上昇0の火力原子力発電所や、CO2排気0の蓄電池駆動自動車類や船舶類にし、利益が少ないと協力不可能なため、利益率抜群の世界一で空気抵抗0CO2排気0の宇宙飛行全盛が必要です。 In existing thermal power nuclear power plants in the world, accelerating CO2 global warming and increasing sea surface temperature by 7 degrees centigrade to 1000 times over 100 years in 100 years, increasing CO2 in the atmosphere global warming accelerating and rising seawater temperature Increase the updraft, increase abnormally dry wildfires and droughts and torrential rains as much as possible, and decrease the land food of humanity as much as possible, and the natural phenomenon of supplying nutrients to the sea surface cooling seabed in the winter, impossible, Reduce phytoplankton, seaweeds, corals, etc., reduce fish to 1/100 by food chain, decrease human food in the sea as much as possible and increase flooding, torrential rain, typhoon, and monsoon by 10 times in 100 years. For example, with typhoons and seasonal winds set at 300 m / s etc., there is a task to prevent global warming and postpone humanity extinction to increase the danger of human extinction, and if fossil fuel is burned in large quantities, the earth warms. As a result, the resource utilization will be depleted, so it will be necessary to minimize the use of fossil fuel combustion as a space utilization prime airplane with zero air resistance and 0 CO2 exhaust, leaving limited resources in the descendants and a thermal power plant with zero sea temperature rise, Since CO2 exhaust 0 can not be used as a storage battery powered automobile or ship, and cooperation can not be achieved if the profit is low, the world's No. 1 CO2 exhaust 0 space drag with excellent air resistance is necessary.
熱製造の熱ポンプを各種太陽熱重力タービンで駆動すると、温熱(過熱蒸気熱量)と冷熱(圧縮空気質量)を燃料費0で無限製造の挑戦となり、重力太陽熱発電や重力太陽エンジンにより、太陽熱や熱製造装置の熱ポンプにより温熱と冷熱の製造量を無限大に近付け、限りある石油資源等は必要最小限の使用とし、子子孫孫まで残すと共に地球温暖化防止して、旱魃や海面上昇や台風や季節風の巨大化を阻止し、海底に冷熱の酸素や窒素やCO2等の栄養分を供給して、植物プランクトンや海草類やサンゴや魚類等を増殖人類の食物を増大し、既存世界の10倍発電量以上として、各種重力発電全盛にし、重力発電蓄電池駆動の各種自動車類全盛や各種船舶類全盛や、電気駆動の全面電化住宅全盛や工場電化全盛や温熱と冷熱利用全盛にして、海水温度上昇0やCO2排気0や燃料費0で発電し、地球温暖化防止の人類絶滅先送りにして、重力太陽熱タービンで温熱や冷熱の製造を無限に継続し、温熱を過熱蒸気50で保存短時間最大熱量噴射を可能として、宇宙上昇時には合体機関噴射部78Wにより短時間噴射推進力を、既存ジェット機の100倍圧力10倍熱量噴射1000倍噴射出力狙いとし、飛行機類は燃料消費が0に近い宇宙利用全盛や成層圏利用全盛にして、宇宙から成層圏飛行時には燃料消費0や僅少で最も効率良く過熱蒸気を製造し、燃料消費僅少で限りある資源を子孫に残す共に、無限大に近い発電は水重力発電にして最も軽量大出力が必要な飛行機類は水銀駆動や衝撃低減タービン駆動にして、空気抵抗0CO2排気0飛行が可能な宇宙飛行全盛にします。 When the heat pump of heat production is driven by various solar thermal gravity turbines, it becomes a challenge of infinite heat production (thermal heat of superheated steam) and cold heat (compressed air mass) with zero fuel cost, and solar heat and heat by gravity solar thermal power generation and gravity solar engine. The heat pump of the manufacturing equipment brings the amount of heat and cold close to infinity, limiting the limited petroleum resources to the minimum necessary use, leaving the children and descendants as well as preventing global warming, rising sea level and typhoon, typhoon And prevent the growth of monsoon winds, supply nutrients such as cold oxygen, nitrogen and CO2 to the bottom of the sea floor, multiply phytoplankton, seaweeds, corals and fish, etc. to increase human food and generate 10 times the power of the existing world More than quantity, various gravity power generation to be full, various vehicles such as gravity power generation storage battery driven various kinds of ships and various ships kindly, electric drive all electrification house fullness and factory electrification fullness and heat and cold heat utilization best We generate electricity with seawater temperature rise 0 and CO2 exhaust 0 and fuel cost 0, and continue the production of heat and cold heat infinitely with the gravity solar heat turbine with the endowment of humanity extinction to prevent global warming, save heat with superheated steam 50 short The maximum amount of thermal energy injection is possible, and during the ascension, the combined engine injection unit 78 W aims to make short-time injection propulsion power 100 times the pressure of existing jets 10 times the amount of thermal energy injection 1000 times injection target. Space use and stratosphere use, and during space-to-stratosphere flight, fuel consumption is zero or minimal, and superheated steam is produced most efficiently, leaving only limited resources for fuel consumption, and generations close to infinity The airplanes that require the greatest light weight and high output for gravity power generation are driven by mercury and impact reduction turbines, and are made to fly in space that can achieve zero air resistance and zero CO2 exhaust.
CO2排気僅少燃料消費僅少の竪型被覆金属球重力衝撃低減タービン8G複数駆動を、熱量タービン駆動と質量タービン駆動とし、宇宙では熱量加速と質量加速に大気中では重力追加駆動で使用して、被覆金属球重力太陽熱エンジン回転出力発生にし、噴射推進出力を既存ジェット機の100倍圧力10倍熱量噴射短時間1000倍噴射推進出力狙いとして、複数の竪型被覆金属球重力衝撃低減タービン8G駆動の被覆金属球重力太陽熱エンジンとし、宇宙では太陽光直射部120度Cと日陰部−150度Cという絶好環境を利用して、過熱蒸気タービン駆動や過熱蒸気製造絶好の環境を利用して、吸入空気路を密閉空気路として圧縮空気減圧して120度太陽光を長レンズ等で回収し、過熱蒸気でタービン駆動熱ポンプにより1200度前後に圧縮空気を圧縮熱交換過熱蒸気製造にして、タービン排気を−150度日陰部で冷却して復水にする循環を繰り返し、通常は燃焼ガス使用0合体機関噴射部78Wより過熱蒸気50のみ噴射する噴射推進出力発生にして、燃料量0で既存ジェットエンジンの10倍噴射推進出力狙いにし、燃料消費僅少として既存世界の各種船舶類や各種飛行機類で宇宙利用全盛を狙う効果と、資源を子孫に残す効果があります。 CO2 emissions Slight fuel consumption Slightly-shaped fuel-class coated metal spheres Gravity impact reduction turbine 8G Multiple drive is used as calorific turbine drive and mass turbine drive, and using gravity additional drive in the atmosphere for thermal energy acceleration and mass acceleration in space Metal ball gravity solar thermal engine rotational power generation, injection propulsion output 100 times pressure 10 times thermal energy injection short time 1000 times injection propulsion output aim of the existing jet machine, a plurality of bowl-shaped coated metal ball gravity impact reduction turbine 8G driven coated metal It is a spherical gravity solar thermal engine, and by utilizing the excellent environment of 120 degrees C of direct sunlight and 150 degrees C of shaded area in space, the intake air path is made use of the superheated steam turbine drive and the superheated steam production excellent environment. Compressed air is decompressed as a closed air path and 120 degree sunlight is collected with a long lens etc., and it is 1200 degrees ago by a turbine drive heat pump with superheated steam The compressed air is compressed heat exchange superheated steam production, and the circulation is repeated to cool the turbine exhaust at the -150 degree shade part to be condensed water, and usually only the superheated steam 50 is injected from the combined combustion engine use part 78W It aims to generate 10% of the amount of fuel by 0% of fuel injection and generate 10% of the amount of fuel by the existing jet engine, and consumes less fuel and aims to use space in various ships and planes of the existing world. There is an effect to leave.
発明の実施の形態や実施例を、図面を参照して説明するが、実施形態や実施例と既説明とその構成が略同じ部分には、同一の名称又は符号を付して、重複説明はできるだけ省略し、特徴的な部分や説明不足部分は、順次追加重複説明する。又非常に難解な脳内理論最良エンジン発明のためと、意図する所及び予想を具体的に明快に説明するため、アイディアを仮説数字で説明するが、正解は実験数字として理論最良エンジンの仮説数字に限定しません。最良と思われるアイディアを多数の用途で重複説明し、用途に合せてアイディアを選択使用して、請求項では多用途に合せて選択使用するため千変万化し、理論最良エンジンから順次噴射推進を含む資源量や需要量に合わせた出力として、例えば無限需要量の発電は水出力や衝撃低減タービン駆動にして軽量大出力が最も重要な飛行機類は水銀出力や衝撃低減タービン駆動とし、軽量大出力が重要な船舶類は鉛合金中核液体金属出力や衝撃低減タービン駆動として、実験最良エンジンに移行実用化します。 The embodiments and examples of the invention will be described with reference to the drawings, but the same names and symbols are given to parts substantially the same as the ones in the embodiments and examples described above. It will be omitted as much as possible, and the characteristic parts and the inexplicable parts will be sequentially added and explained. In addition, although the idea is explained with hypothesized numbers in order to clearly explain the intended purpose and prediction specifically for the extremely difficult brain theory best engine invention, the correct answer is the experimental number of the theoretical best engine as the experimental number. Not limited to The idea that seems to be the best is redundantly explained in many applications, and the idea is selected and used according to the application, and the claim is converted into a variety for selection and use according to the versatility, resources from theoretical best engine to sequential injection promotion As output according to the volume and demand volume, for example, power generation with infinite demand is driven by water output and impact reduction turbine, and light and large output is most important airplanes with mercury output and impact reduction turbine drive, light and large output is important Marine vessels will be put to practical use as the lead engine core liquid metal power and impact reduction turbine drive, etc.
図1の竪型被覆金属球重力衝撃低減太陽熱温熱タービン8Gは、タービン翼角度を衝撃に強い角度として、金属球使用では合成樹脂等弾力性弾性材料の被覆を設け、被覆金属球使用では鏡面等として衝撃低減タービン翼摩耗防止とし、増大球上昇装置2Fを設けて被覆金属球を最上部に上昇保存して、外箱77a内に1〜10段等タービンを垂直に多段に設けて用途に合わせた台数使用にし、1種類使用では温熱タービン8G冷熱タービン8G選択使用として、2種類使用は温熱タービン+冷熱タービン使用にし、被覆金属球を金属噴射ポンプ6M等で噴射して過熱蒸気温熱加速重力加速度加速して、竪型被覆金属球重力衝撃低減太陽熱温熱タービン8Gを駆動し、タービン間に横軸1hを設けてタービン外箱77a外で、発電機1や熱ポンプ1Gや圧縮熱回収器2Cや水熱交換器2Yや空気熱交換器2Xを駆動して、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、太陽熱を種に熱ポンプ1Gと圧縮熱回収器2Cで無限大に近い温熱(圧縮空気熱量の過熱蒸気)や冷熱(圧縮空気質量)を製造して、例えば500度前後24〜400MPa過熱蒸気温熱+100ヘ200度前後24〜400MPa圧縮空気冷熱に分割保存し、一部と重力で温熱タービン+冷熱タービンを駆動して、大部分で合体機関噴射部78Wを駆動太陽熱重力ヘリコプター39C飛行にし、停止中は熱と電気の供給設備等で使用します。 The vertical-coated metal ball gravity impact reduction solar thermal thermal turbine 8G of FIG. 1 is provided with a coating of a resilient elastic material such as a synthetic resin when using a metal ball, with the turbine blade angle as a strong angle to impact, and a mirror surface etc. when using a coated metal ball As an impact reduction turbine blade wear prevention, increase ball lifting device 2F is provided and the coated metal balls are raised and stored at the top, and turbines of 1 to 10 stages etc. are vertically provided in multistage in outer box 77a to fit the application In one kind of use, use one kind of thermal turbine 8G cold heat turbine 8G as selection use, use two kinds of thermal heat turbine + cold heat turbine, and spray coated metal balls by metal injection pump 6M etc. to overheat steam thermal acceleration gravity acceleration Accelerating and driving the vertical coated metal ball gravity impact reduced solar thermal thermal turbine 8G, providing horizontal axis 1h between the turbines, outside the turbine outer box 77a, the generator 1, heat ponpo Drives 1G, compression heat recovery unit 2C, water heat exchanger 2Y and air heat exchanger 2X, alternates the rotational direction of turbine 8G, offsets vibration and noise slightly, and compresses heat pump 1G and compression using solar heat as a seed Thermal heat (compressed air heat superheated steam) and cold heat (compressed air mass) close to infinity are produced by heat recovery unit 2C, for example, around 500 degrees 24 to 400 MPa overheated steam thermal + 100 ° around 200 degrees 24 to 400 MPa compressed air Split and store in cold heat, drive thermal turbine + cold heat turbine with a part and gravity, drive united engine injection part 78W in most part to make it a solar thermal gravity helicopter 39C flight, and use it for supply equipment of heat and electricity while stopping To do.
温熱タービン8G駆動の過程では、冷熱タービン8Gで冷却した被覆金属球を500度前後過熱蒸気50で加熱温度上昇して、冷熱タービン駆動圧縮空気冷熱容積増大にして回転出力を増大し、冷熱タービン排気を合流抽出器51で吸入して、低圧冷熱にして合体機関噴射部78Wの最適圧力冷熱に合流酸化剤で使用する循環にし、温熱タービン排気の過熱蒸気も合流抽出器51で、合体機関噴射部78Wの最適圧力温熱に合流推進剤で使用して、内側動翼群60C外側動翼群60Dは大重量を支える油圧浮上追加の推力軸受80aを具備し、全自動加工可能に段落毎同径略同形として嵌合ボルト組立にして、多段動翼群と多段タービンを可能にすると共に組立容易にし、被覆金属球を加速する重力加速部1gには横軸1hや貫通穴を具備して、発電機1や熱ポンプ1G多数等をタービン外箱77aの外で駆動し、太陽熱加熱の空気を圧縮1000度前後にして、空気熱交換器2Xで太陽熱加熱の別空気を600度C等に加熱して圧縮1200度前後にし、繰り返して高圧の圧縮空気28a冷熱と過熱蒸気50温熱の熱製造量を増大して、大気圧同速度同容積仕事率kg重m/秒最高を、既存蒸気タービンの3.6万倍前後白金球仕事率等にし、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射して、転がり接触回転出力発生で重力や太陽熱を最大限利用し、圧縮空気冷熱製造と温熱(過熱蒸気)を製造する、竪型被覆金属球重力衝撃低減太陽熱温熱タービン8Gにします。 In the process of thermal turbine 8G drive, the coated metal spheres cooled by the cold turbine 8G are heated by the 500 ° C superheated steam 50 and the heating temperature is raised to increase the cooling air volume of the cold air driven compressed air to increase the rotational output, and the cold heat turbine exhaust Is drawn by the combined extraction unit 51, turned into low pressure cold, and used as a combined oxidizing agent for optimum pressure cooling of the combined engine injection unit 78W, and superheated steam of the thermal turbine exhaust is also combined by the combined extraction unit 51, combined unit injection unit Used with combined propellant for optimum pressure and heat of 78 W, inner rotor blade group 60C outer rotor blade group 60D has additional hydraulic levitation additional thrust bearing 80a to support heavy weight, and can be machined automatically with almost the same diameter for full automatic machining The same type of fitting bolt assembly enables multistage moving blade group and multistage turbine as well as easy assembly, and the gravity acceleration part 1g for accelerating coated metal balls has a horizontal axis 1h and a through hole Drive a large number of generators 1, heat pumps 1G, etc. outside the turbine outer box 77a, compress the air of solar heating to about 1000 degrees, and separate the air of solar heating to 600 degrees C, etc. with the air heat exchanger 2X. Heat to compression around 1200 degrees, repeatedly increase the heat production of high pressure compressed air 28a cold energy and superheated steam 50 thermal energy, atmospheric pressure same speed same volume work ratio kg weight m / s maximum, existing steam turbine The platinum blade power factor of around 36,000 times that of 2 and the cross section of the existing turbine blade is made 2 to 26 times the cross sectional area of the turbine blade cross section 4X and injected to the blade cross section 4X to maximize the use of gravity and solar heat by rolling contact rotational power generation And, to produce the compressed air cold heat production and heat (superheated steam), the vertical coated metal ball gravity impact reduced solar thermal turbine 8G.
図2の竪型被覆金属球重力衝撃低減太陽熱冷熱タービン8Gも、タービン翼角度を衝撃に強い角度として、金属球使用では合成樹脂等弾力性弾性材料の被覆を設け、被覆金属球使用では鏡面等として衝撃低減タービン翼摩耗防止とし、外箱77a内に1〜10段等タービンを垂直に多段に設けて、用途に合わせた台数使用にして、温熱タービン駆動で温度上昇した被覆金属球を増大球上昇装置2Fで最上部に上昇保存し、被覆金属球を金属噴射ポンプ6M等で噴射して圧縮空気28a冷熱加速重力加速度加速して、竪型被覆金属球重力衝撃低減太陽熱冷熱タービン8Gを被覆金属球の転がり接触で駆動し、駆動の過程で絶対0度に近付く圧縮空気28aを温度上昇した被覆金属球で加熱して、圧縮空気容積速度を増大してタービン出力を増大して被覆金属球を冷却し、冷却した被覆金属球で温熱タービン8G駆動被覆金属球温度を上昇する循環として、温度上昇した冷熱タービン排気を合流抽出器51で吸入低圧冷熱として出力増大にし、燃料費0の被覆金属球重力タービンによる圧力上昇にして、合体機関噴射部78Wの最適圧力冷熱に合流酸化剤で使用する循環にし、圧縮空気冷熱の最大限活用にします。 The vertical-type coated metal ball gravity impact reduction solar thermal cold turbine 8G of FIG. 2 also uses the metal ball use a coating of a resilient elastic material such as a synthetic resin when the turbine blade angle is a strong angle to impact, and a mirror surface etc. As the impact reduction turbine blade wear prevention, 1 to 10 stages etc. turbines are vertically installed in multi-stage vertically in the outer box 77a, and the number increase according to the application is used. Lifting and storing at the top with the lifting device 2F, the coated metal ball is sprayed by the metal injection pump 6M etc. and compressed air 28a cold thermal acceleration Gravity acceleration is accelerated, and the vertical coated metallic ball gravity impact reduced solar thermal cold turbine 8G coated metallic Drive with rolling contact of balls and heat compressed air 28a which approaches absolute zero in the process of driving with coated metal balls at elevated temperature to increase compressed air volume velocity and increase turbine output The coated metal balls are cooled, and the cooled coated metal balls are circulated to raise the temperature of the coated metal balls by raising the temperature of the coated metal balls. The pressure is raised by the coated metal ball gravity turbine of 0, and it is used for the optimum pressure cooling of the combined engine injection part 78W with the combined oxidant, and it makes the best use of the compressed air cooling.
タービン間重力加速部1gに貫通穴と横軸1hを設けタービン外箱77a外で、発電機1や熱ポンプ1Gや圧縮熱回収器2Cや水熱交換器2Yや空気熱交換器2X等を駆動して、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、太陽熱を種に熱ポンプ1Gと空気熱交換器2Xで無限大に近い温熱や冷熱を製造して、24〜400MPa過熱蒸気温熱+24〜400MPa圧縮空気冷熱に分割保存使用し、圧縮空気28a冷熱で被覆金属球を加速駆動する、竪型被覆金属球重力衝撃低減太陽熱冷熱タービン8Gにして、内側動翼群60C外側動翼群60Dには、大重量を支える油圧浮上追加の推力軸受80aを具備して多段タービンを可能にし、太陽熱加熱の空気を圧縮1000度前後にして、空気熱交換器2Xで太陽熱加熱の別空気を500度C等に加熱して圧縮1200度前後にし、繰り返して高圧の圧縮空気28aと過熱蒸気50の製造量を増大するエネルギ保存サイクルにして、大気圧同速度同容積仕事率kg重m/秒最高を、既存蒸気タービンの3.6万倍前後白金球仕事率にし、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射して、転がり接触回転出力発生とし、重力や太陽熱を最大限利用する、竪型被覆金属球重力衝撃低減太陽熱冷熱タービン8Gにします。 A through hole and horizontal axis 1h are provided in the inter-turbine gravity acceleration unit 1g, and the generator 1, heat pump 1G, compression heat recovery device 2C, water heat exchanger 2Y, air heat exchanger 2X, etc. are driven outside the turbine outer box 77a. Then, the rotational direction of the turbine 8G is alternated to offset the vibration and noise slightly, and the solar heat is used as a heat pump 1G and the air heat exchanger 2X to produce nearly infinite heat and cold, 24 to 400MPa heating Steam heat +24-400MPa compressed air cold storage divided use, compressed air 28a cold heat accelerating coated metal spheres, vertical type coated metal ball gravity impact reduced solar thermal cold turbine 8G, inner rotor blade group 60C outer rotor blade The group 60D is equipped with a hydraulic levitation additional thrust bearing 80a to support a large weight to enable a multi-stage turbine to compress the air of solar heating to about 1000 degrees, and heat the solar heating with the air heat exchanger 2X Separate air is heated to 500 ° C, etc. and compressed to around 1200 ° C, and it is an energy storage cycle that repeatedly increases the production volume of high pressure compressed air 28a and superheated steam 50, atmospheric pressure same speed same volume work power kg weight The rolling contact rotational power is generated by injecting the m / s maximum into the turbine blade cross section 4X, which has a platinum ball power factor of around 36,000 times that of the existing steam turbine and a cross section of 2 to 26 times the existing turbine blade cross section And, to make the best use of gravity and solar heat, we will make a solar-heat-heat turbine 8G vertical-type coated metal ball gravity impact reduction solar heat.
図3の合体機関噴射部78W太陽熱重力ヘリコプター39C回転出力噴射推進出力発生は、重力使用が限定されるため飛行胴38a船体10を一体として、図1図2複数竪型被覆金属球重力衝撃低減タービン8G台数選択使用で落差を最適にし、空気吸入口28Bより空気28aを吸入の過程で、長レンズ2d熱吸収材2Bで構成の吸入空気路28Aで太陽熱加熱の空気28aを吸入して、熱ポンプ1Gで圧縮1000度等にして空気熱交換器2Xで太陽光加熱の別空気28aで熱回収し、熱ポンプ1Gで圧縮1200度等として熱回収を繰り返す圧縮熱製造として、水熱交換器2Yでは過熱蒸気50製造で熱回収を繰り返す熱製造とし、宇宙上昇時には圧縮熱回収器2Cで燃料噴射燃焼限り無く高圧燃焼熱交換冷却燃焼して、繰り返し圧縮1200度等にして水熱交換器2Yで熱回収を繰り返して、過熱蒸気50と燃焼ガス49質量を、既存ジェット機噴射圧力の10〜100倍圧力等で合体機関噴射部78Xに供給し、燃焼ガス49に燃料噴射燃焼外周の過熱蒸気50を加熱全部で10倍熱量等を噴射して、噴射推進出力を既存ジェット機の100〜1000倍に短時間近付けて宇宙に到達し、宇宙では超音速マッハ32の地球脱出速度や光の速度に近付けて、各種飛行船舶類や各種航空機類で燃料費0に近い宇宙利用全盛にし、中間圏飛行や成層圏飛行を可能にして、大気中では複数回転翼7Bを夫々の1〜3.6万倍仕事率タービンで回転駆動飛行し、圧縮空気28a酸化剤冷熱と過熱蒸気50推進剤温熱を貯蔵増大し、大出力ロケット推進の準備をします。 The combined engine injection unit 78 W solar thermal gravity helicopter 39C rotational output injection propulsion output generation of FIG. 3 integral with the flight shell 38a hull 10 because gravity use is limited, FIG. The drop is optimized by the selective use of the 8G number, and in the process of suctioning the air 28a from the air suction port 28B, the solar heating air 28a is suctioned by the suction air passage 28A composed of the long lens 2d heat absorbing material 2B. In the water heat exchanger 2Y, compression heat production is repeated by setting the compression to 1000 degrees at 1 G, recovering heat with another air 28a of solar heating with the air heat exchanger 2X, and performing heat recovery as the compression 1200 degrees with the heat pump 1G. Heat production is repeated by heat recovery in the production of superheated steam 50. When rising up in space, high pressure combustion heat exchange cooling combustion is carried out by the compression heat recovery unit 2C as much as fuel injection combustion is possible, and repeated compression is performed. Heat recovery is repeated with the water heat exchanger 2Y at 200 degrees etc., and the superheated steam 50 and the combustion gas 49 mass are supplied to the combined engine injection part 78X at a pressure 10 to 100 times the existing jet injection pressure, etc. The heat is injected 10 times in total by heating the superheated steam 50 on the outer periphery of the fuel injection and combustion, and the injection propulsion output approaches the 100 to 1000 times of the existing jet for a short time to reach space, and supersonic Mach 32 in space Approach the speed of the Earth's escape and the speed of light, make it possible to use the space with a fuel cost close to zero with various types of flight vessels and aircraft, enable mesosphere flight and stratosphere flight, and make multiple rotors 7B in the atmosphere. Each 1 to 36,000 times work rate rotary driven flight, compressed air 28a oxidizer cold heat and superheated steam 50 storage storage increase, prepare for high power rocket propulsion.
大気中を飛行時には複数の竪型被覆金属球重力衝撃低減タービン8G駆動の、回転翼7B複数の回転出力により垂直上昇降下海上陸上何処でも着水着陸可能に飛行し、熱ポンプ1G・圧縮熱回収器2C・空気熱交換機2X・水熱交換器2Yを、横並び又は立て並びタービン横軸1h駆動として、用途に合わせた台数を夫々1〜10段に設けて落差を増大し、被覆金属球を金属噴射ポンプ6M等で噴射して、分割保存した圧縮空気冷熱+圧縮空気温熱で加速し、夫々の竪型被覆金属球重力衝撃低減タービン8Gに噴射して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にし、タービン翼8cに噴射転がり接触駆動で重力や太陽光を最大限利用して、大気圧同速度同容積仕事率kg重m/秒最高を、既存蒸気タービンの3.6万倍前後白金球仕事率にし、熱ポンプ多数を重力太陽熱駆動して、24〜400MPa過熱蒸気50温熱と24〜400MPa圧縮空気28a冷熱を限り無く増大し、空気吸引噴射推進する出力の発生は、合体機関噴射部78Wに分割保存した過熱蒸気50と圧縮空気49を供給して、燃料噴射燃焼双方の噴射温度を近付けることで理論最良の噴射とし、既存ジェット機の10〜100倍圧力1/10噴射熱量10倍噴射推進出力大型化等として、船体10の外部に複数〜多数設けた、合体機関噴射部78Wを180度以上回転して逆噴射や垂直上昇垂直降下を可能にし、宇宙利用全盛や水上等何処でも着水着陸可能にして、月面着陸等の場合は4脚や6却等を設けて着陸可能にします。 When flying in the atmosphere, multiple vertical-type coated metal sphere gravity impact reduction turbine 8G driven, rotary rising power of rotary wings 7B by multiple rotary powers enables vertical landing and landing on land anywhere possible to fly, heat pump 1G, compression heat recovery 2C · air heat exchanger 2X · water heat exchanger 2Y in a row or in a row with turbine horizontal axis 1h drive, provide 1 to 10 stages according to the application to increase the head and make the coated metal balls metal Sprayed by injection pump 6M etc., accelerated by compressed air cold heat + compressed air thermal energy stored separately, and injected to each vertical coated metal ball gravity impact reduction turbine 8G, turbine blade cross section 4X to existing steam turbine 2 Up to 26 times, maximum utilization of gravity and sunlight by injection rolling contact drive to turbine blade 8c, atmospheric pressure same speed same volume work power kg weight m / s maximum, 36,000 times of existing steam turbine Front and back white With the power of spheres, heat pumps are driven by gravity solar heat, and 24 to 400 MPa superheated steam 50 thermal energy and 24 to 400 MPa compressed air 28a cold heat is increased without limit, and the generation of air suction injection and propulsion output is the united engine injection part Supply the superheated steam 50 and compressed air 49 separately stored at 78 W, and make the injection temperature of both fuel injection and combustion close to the theoretical best injection, 10 to 100 times the pressure of the existing jet, 1/10 injection heat quantity 10 times injection In order to make the propulsion output larger, etc., the combined engine injection unit 78W provided outside the hull 10 is rotated 180 degrees or more to enable reverse injection or vertical rise and vertical descent, and it can be worn anywhere, such as in space use or water Water landing is possible, and in the case of moon landing etc., landing is possible by setting 4 legs or 6 turns.
宇宙到達時前に回転翼7Bを停止して、冷熱駆動竪型被覆金属球重力衝撃低減タービン8G駆動の排気を空気抽出器51で吸入の過程で、空気路入口28Bを密閉冷熱タービン8Gの圧縮空気28a排気により、120度直射太陽光の熱量を長レンズ2d熱吸収材2B空気28a排気で熱回収し、500度前後排気を温熱タービン駆動と冷熱タービン駆動多数の熱ポンプ1Gで圧縮して、1200度前後にして空気熱交換器2Xで太陽光加熱の別空気28aで熱交換熱回収し、熱ポンプ1Gで圧縮1200度等にして熱回収と冷熱タービン駆動を繰り返して、同様に水熱交換器2Yでは過熱蒸気50製造と温熱タービン駆動を繰り返し、宇宙では過熱蒸気50温熱を120度直射太陽光で最も効率良く製造貯蔵して、温熱タービン8Gや冷熱タービン8Gを温熱駆動や冷熱駆動重力0に対応し、宇宙での噴射推進は過熱蒸気50推進材による噴射推進とし、圧縮空気28aは過熱蒸気50の製造や生命維持物質で使用して、長距離の宇宙旅行を可能にし、地球帰還時には摩擦熱を含む高圧高温空気28aを吸入圧縮熱交換する熱製造にして、圧縮空気28a冷熱で冷熱タービン8Gを駆動し、その排気を合流抽出器51により吸入最適圧力に圧縮して、合体機関噴射部78W酸化剤の最適圧力部に合流し、燃料噴射着火燃焼噴射推進出力の増大に使用します。 The rotor 7B is stopped before reaching the space, and in the process of sucking the exhaust of the cold heat-driven cage type coated metal ball gravity impact reduction turbine 8G drive by the air extractor 51, the air passage inlet 28B is compressed the closed cold heat turbine 8G. The heat of 120 ° direct sunlight is recovered by the air 28a exhaust, the heat is recovered by the long lens 2d heat absorbing material 2B air 28a, and the exhaust around 500 degrees is compressed by the heat turbine drive and the large number of heat pump drives 1G. Heat exchange heat recovery with another air 28a of solar heating with air heat exchanger 2X at around 1200 ° C, compression with heat pump 1G to 1200 ° C etc. Heat recovery and cold heat turbine drive are repeated, and water heat exchange similarly In the unit 2Y, superheated steam 50 production and thermal turbine drive are repeated, and in the space, the superheated steam 50 temperature is produced and stored most efficiently by direct sunlight at 120 degrees, and the thermal turbine 8G and the cold energy -Corresponds to thermal drive and cold drive gravity 0, bin 8G uses injection propulsion by superheated steam 50 propellant as space jet propulsion and compressed air 28a is used for manufacturing superheated steam 50 and life support material, long distance Space travel is made possible, and high pressure high temperature air 28a including frictional heat is suctioned and compressed and heat-exchanged during the earth return to produce heat to drive cold heat turbine 8G with cold air of compressed air 28a. It is compressed to the optimum pressure, joined to the optimum pressure part of the combined engine injection part 78W oxidant, and used to increase the fuel injection ignition combustion injection propulsion output.
図4の合体機関噴射部78W駆動は、過熱蒸気制御弁25を開放分割保存した過熱蒸気50を燃焼器1Y外周の過熱蒸気溜95cの最上流に供給し、宇宙上昇準備の場合は推進剤の過熱蒸気50製造の過程で圧縮空気28aに燃料噴射燃焼して、圧縮熱回収器2Cで複数回圧縮燃料噴射燃焼複数回熱回収し、限り無く高圧の燃焼ガス49酸化剤と過熱蒸気50推進剤を貯蔵限り無く増大して、宇宙上昇時には燃焼ガス制御弁24を開放し、200度前後24〜400MPa燃焼ガス49を燃焼ガス溜95a燃焼器1Yの最上流に供給して、燃料制御弁25b開放燃料噴射ポンプ1Dにより燃料1bを燃料噴射ノズル6Xより噴射し、燃焼器1Y最上流で着火燃焼外周の過熱蒸気50を加熱燃焼温度を上昇して、外周長大な過熱蒸気溜95cの400度前後24〜400MPa過熱蒸気50を加熱双方の噴射出力を増大し、燃焼器1Yの複数燃焼ガス噴射ノズル6Yを過熱蒸気溜95c外周に具備して、1段噴射燃焼流の中に夫々の燃料噴射ノズル6Xより燃料噴射2段燃焼器複数最適距離燃焼にし、過熱蒸気50を外周より加熱して噴射出力と燃焼ガス吸引出力を増大して、過熱蒸気50噴射流に複数の燃焼器燃焼ガス噴射ノズル6Yを具備し、夫々の燃料噴射ノズル6Xより燃料噴射3段燃焼器複数最適距離環状燃焼にして、過熱蒸気50噴射流を内周と外周から環状加熱し、100度Cに近付く過熱蒸気を500度等として、既存ジェット機の10〜100倍圧力10倍質量噴射の安価な噴射出力狙いにします。 The united engine injection unit 78W drive shown in FIG. 4 supplies the superheated steam 50 with the superheated steam control valve 25 opened and divided and stored in the uppermost stream of the superheated steam reservoir 95c on the outer periphery of the combustor 1Y. Fuel is injected into compressed air 28a in the process of producing superheated steam 50, and the heat is recovered multiple times by compressed heat recovery device 2C and compressed fuel injection combustion multiple times, and heat is recovered a number of times, infinitely high pressure combustion gas 49 oxidant and superheated steam 50 propellant As much as possible for storage, open the combustion gas control valve 24 at the time of ascent, and supply combustion gas 49 around 200 degrees to the uppermost stream of the combustion gas reservoir 95a combustor 1Y to open the fuel control valve 25b. The fuel 1b is injected from the fuel injection nozzle 6X by the fuel injection pump 1D, and the overheated steam 50 of the ignition combustion outer periphery is heated in the uppermost stream of the combustor 1Y by heating to increase the combustion temperature, Increase the injection output of both heating by heating the superheated steam 50 around 24-00MPa around 00 degrees, equipped with the multiple combustion gas injection nozzle 6Y of the combustor 1Y on the outer periphery of the superheated steam reservoir 95c, into each one-stage injection combustion flow The fuel injection two-stage combustor multiple optimal distance combustion from the fuel injection nozzle 6X, and the superheated steam 50 is heated from the outer periphery to increase the injection output and the combustion gas suction output, and a plurality of combustor combustion gases to the superheated steam 50 injection flow The superheated steam which is equipped with the injection nozzle 6Y and annularly heats the superheated steam 50 injection stream from the inner circumference and the outer circumference by annular combustion from the fuel injection nozzle 6X to the fuel injection three-stage combustor multiple optimal distance The aim is to use an inexpensive jet output of 10 to 100 times the pressure and 10 times the mass of the existing jet, with 500 degrees etc.
過熱蒸気50の低温噴射大膨張速度と燃焼ガス49の高温噴射を合体して、夫々の長所を利用最良の組み合わせにした理論最良の合体機関噴射部78Wとし、既存のスクラムジェット高速燃焼と蒸気タービンの高圧噴射を合体高温高圧噴射にして、大気中を飛行時には圧縮熱回収器2Cの燃焼が不要で、上記燃焼ガス制御弁24開放が圧縮空気制御弁24A開放となり、太陽光加熱の空気28aを圧縮酸化剤製造し、1000度等に圧縮して圧縮熱回収器2Cで熱交換過熱蒸気50の推進剤製造にして、推進剤と酸化剤を保存増大主として過熱蒸気50による噴射推進とし、1段燃焼も2段燃焼も3段燃焼も僅少にする地球温暖化防止推進として、100度に近付く過熱蒸気50を500度等に加熱噴射推進出力を大幅に増大し、過熱蒸気容積の大部分を増大噴射速度を増大燃焼ガス49の吸引力を増大して、最も効率良く過熱蒸気50と燃焼ガス49を混合噴射する合体機関噴射部78Wを駆動し、既存スクラムジェット高速燃焼+蒸気タービンの高圧噴射大膨張速度として、過熱蒸気50や燃焼ガス49や圧縮空気28aの酸化剤や推進剤を保存使用し、円筒回転部77Gを180度以上の回転にして垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や宇宙利用全盛にし、地球上何処でも日帰り旅行等を可能にします。 Combined low-temperature injection of superheated steam 50 and high-temperature injection of combustion gas 49 into the theoretical best combination engine injection part 78 W that makes the best combination by utilizing the respective merits, existing scramjet high speed combustion and steam turbine The high-pressure injection is integrated into the high-temperature and high-pressure injection, and the combustion of the compression heat recovery unit 2C is unnecessary when flying in the atmosphere, and the combustion gas control valve 24 is opened to open the compressed air control valve 24A, and the solar heating air 28a is Produces compressed oxidant, compresses it to 1000 ° C, etc. and makes it into a propellant of heat exchange superheated steam 50 with compression heat recovery device 2C, increases the storage of propellant and oxidizer mainly by injection promotion by superheated steam 50, 1 step In order to prevent global warming, where combustion and two-stage combustion and three-stage combustion are minimal, the superheated steam 50 approaching 100 degrees is heated up to 500 degrees etc. Increase the injection speed Increase the suction power of the combustion gas 49, drive the combined engine injection part 78W that mixes and inject the superheated steam 50 and the combustion gas 49 most efficiently, existing scramjet high speed combustion + steam As the high-pressure injection large expansion speed of the turbine, the oxidant and propellant of superheated steam 50, combustion gas 49 and compressed air 28a are stored and used, and the cylinder rotation part 77G is rotated by 180 degrees or more, and vertical rise, vertical drop, reverse It enables injection and makes it possible to fly anywhere on the airfield and space use, and enables day trips etc. anywhere on the earth.
理論最良タービンの竪型被覆金属球重力衝撃低減太陽熱温熱タービン8G+竪型被覆金属球重力衝撃低減太陽熱冷熱タービン8Gとして、太陽熱加熱の空気を熱ポンプで吸入圧縮熱回収して24〜400MPa等の温熱+冷熱で保存使用し、タービン駆動合体機関噴射部78W太陽熱重力ヘリコプター39Cとして、垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や宇宙利用全盛にし、地球上何処でも日帰り旅行等を可能にする可能性があります。 Theoretical best turbine Vertical-type coated metal ball Gravity impact reduction solar thermal thermal turbine 8G + vertical-type coated metal ball gravity impact reduction solar thermal cold thermal turbine 8G, solar thermal air with heat pump suction suction compression heat recovery and thermal temperature such as 24-400MPa + Save as cold, use as a turbine drive united engine injection unit 78 W solar thermal gravity helicopter 39C, enable vertical ascent and vertical descent and reverse injection, make airfields and space use prime everywhere, day trips etc. anywhere on earth There is a possibility to make it possible.
0:真空、 1:発電機、 1A:水銀排気検査室、 1B:酸素量増大手段、 1C:アルコール冷熱、 1D:燃料噴射ポンプ、 1F:復水ポンプ、 1G:熱ポンプ、 1H:揚水ポンプ、 1J:揚水装置、 1Y:燃焼器、 1b:燃料、 1c:比重大物質、 1d:水銀、 1e:被覆鋼球(衝撃低減手段2Gで被覆) 1e:被覆水銀(球形のステンレス等耐久材や衝撃低減手段2Gで被覆) 1g:重力加速部、 1h:横軸、 2:太陽光加熱器(長レンズで太陽光を傾斜回転して追跡) 2a:水復水器、 2a:復水冷却器、 2b:太陽熱増大吊橋(吊具左右を上下して長レンズ複数段で太陽光を傾斜回転して追跡) 2c:断熱材、 2d:長レンズ、 2e:水面、 2f:吊具左、 2g:吊具右、 2h:海水冷却器、 2z:太陽熱空気加熱器、 2A:耐熱材、 2B:熱吸収材、 2C:圧縮熱回収器、 2D:出力増大手段、 2E:出力増大球(液体鉛や液体錫や液体亜鉛等の液体金属・白金球や被覆白金球や金球や被覆金球や白金合金球や金合金球や鉛合金球や銀合金球や被覆白金合金球や被覆金合金球や被覆鉛球や被覆銀合金球やタングステン合金球や被覆タングステン合金球やタングステン鋼球や被覆タングステン鋼球やタンタル合金球や被覆タンタル合金球やモリブデン鋼球や被覆モリブデン鋼球やモリブデン鋳鉄球や被覆モリブデン鋳鉄球や銀球や被覆銀球等の金属球や被覆金属球) 2F:増大球上昇装置、 2G:衝撃低減手段(小径球・潤滑油類・不燃液体類・ゴム類・プラスチック類等の被覆) 2H:冷熱復水器、 2J:液体金属熱交換器、 2K:潤滑性材料、 2X:空気熱交換器、 2Y:水熱交換器、 2Z:水銀熱交換器、 3:摩擦損失低減手段(撥水作用や加熱高温手段や被覆等最適利用公知技術で摩擦損失を低減) 3A:撥水作用(水との摩擦損失低減手段) 3B:加熱高温手段(電気抵抗や電磁加熱等既存技術で高温にする) 3C:冷熱回収手段、 3E:衝撃低減材料(水銀・液体金属・水) 3G:撥水作用(水銀との摩擦損失低減手段) 4A:タービン翼断面(既存断面) 4B:タービン翼断面(出力面湾曲少断面) 4C:タービン翼断面(出力面直線断面) 4D:タービン翼断面(出力反対面直線断面) 4E:タービン翼断面(出力反対面湾曲少断面) 4F:タービン翼断面(既存の反対断面) 4X:タービン翼断面(4A〜4Fより選択断面) 5C:空気排気室、 6:ノズル、 6a:ノズル噴射部、 6b:ノズル噴射部、 6d:ノズル噴射部、 6z:水噴射ポンプ、 6A:過熱蒸気噴射ノズル、 6B:液体鉛噴射ポンプ、 6C:液体錫噴射ポンプ、 6D:液体ビスマス噴射ポンプ、 6E:液体亜鉛噴射ポンプ、 6F:圧縮空気噴射ノズル、 6H:液体カドミウム噴射ポンプ、 6I:液体インジウム噴射ポンプ、 6J:液体ガリウム噴射ポンプ、 6K:液体タリウム噴射ポンプ、 6L:液体金属噴射ポンプ、 6M:金属噴射ポンプ、 6X:燃料噴射ノズル、 6Y:燃焼ガス噴射ノズル、 6Z:水銀(液体金属)噴射ポンプ、 7:燃料噴射弁、 7A:回転翼7B:回転翼7B、 7C:スクリュー、 7E:回転腕翼、 8a:全動翼弾み車ガスタービン、 8b:全動翼弾み車水タービン、 8c:タービン翼、 8d:側板、 8e:円筒胴、 8E:全動翼弾み車水銀タービン、8F:全動翼弾み車重力タービン、 8G:竪型全動翼被覆金属球重力太陽熱タービン、 8K:液体金属重力対向タービン、8K:対向直列全動翼弾み車タービン、 8L:直列全動翼弾み車タービン、 10:船体、 10A:船室、 10a:拡径圧縮室、10b:操縦室、 10c:制御室、 10d:客室、 10e:貨物室、 11A:隔壁、 11B:水室 11C:空気室、 11D:真空室、 16:クランク軸、16A:水平軸、 21:拡径ピストン、24:燃焼ガス制御弁、 24A:圧縮空気制御弁、 25:過熱蒸気制御弁、 25B:高温水制御弁、 25a:吸気弁、 25b:燃料制御弁、 28a:空気、 28a:内部空気、 28a:空気管空気、 28b:圧縮空気熱量、 28A:吸入空気路、 28B:空気路入口、 37a:着磁摩擦車、 37b:内着磁摩擦車、 38a:飛行胴、 38b:飛行翼、 38c:飛行尾翼、 38d:垂直翼、 38e:翼前縁心、 38g:水上翼、 38h:浮上艇、 38A:重力飛行機、 38B:空気吸引噴射ウォータージェット船舶、 38C:水吸引噴射船舶、 39A:太陽熱重力ヘリコプター39C:合体機関噴射部78W太陽熱重力飛行機、 39B:太陽熱重力ヘリコプター39C:液体金属重力太陽熱飛行機、 39C:太陽熱重力ヘリコプター、 39C:液体金属重力太陽熱飛行船舶、 39C:金属球水重力太陽熱飛行船舶、 39D:スクリュー船舶、 39D:液体金属重力太陽熱船舶、 39F:太陽熱重力飛行機、 39G:太陽熱重力飛行船舶、 39C:飛行船舶、 40A:方向舵、 46:磁石部、 49:燃焼ガス、 49B:煙突燃焼ガス熱量、 49C:工場使用熱量、 50:過熱蒸気、 51:空気抽出器、 51:合流抽出器、 52a:水、 52b:水(太陽光で温度が変る水) 52b:高温水、 52d:温熱、 52d:水温熱、 52d:過熱蒸気温熱、 52e:冷熱、 52e:水冷熱、 52e:圧縮空気冷熱、 52e:アルコール冷熱、 52e:氷冷熱、 55:歯車式同期装置(磁気摩擦同期装置を含む) 55B:磁気摩擦変速装置(歯車式及び送水ポンプ兼用を含む) 55Y:歯車式変速装置(既存変速機から選択) 60A:内側軸装置、 60B:外側軸装置、 60C:内側動翼群、 60D:外側動翼群、 77B:筒形外箱、 77D:ウォータージェット外箱、 77F:噴射部外箱、 77G:円筒回転部、 77a:タービン外箱、 78A:合体機関噴射部、 78B:合体機関噴射部、 78K:合体機関噴射部、 78S:合体機関噴射部、 78T:合体機関噴射部、 78U:合体機関噴射部、 78V:合体機関噴射部、 78W:合体機関噴射部、 78X:合体機関噴射部(78S78T78U78Wがら選択) 79K:合体機関噴射部、 79M:ウォータージェット、 79S:ウォータージェット、 79T:ウォータージェット、 79U:ウォータージェット(水吸引噴射) 79V:ウォータージェット(79S79Tから選択) 79X:ウォータージェット(水吸引噴射) 79Y:ウォータージェット(空気吸引噴射) 79Z:ウォータージェット(空気吸引噴射) 80:軸受、 80a:推力軸受、 80A:継手、 80B:締付具、 81:支軸、 81a:支点、 84:二重反転磁気摩擦動力伝達装置(歯車式及び送水ポンプ兼用を含む) 84Y:二重反転歯車装置(既存技術) 94:固定外箱、 94A:外箱垂直部、 95:高温水溜、 95a:燃焼ガス溜、 95b:圧縮空気溜、 95c:過熱蒸気溜、 95A:吸水路、 95B:燃料溜、 96A:送水路、 97:逆止弁、103:冷熱回収器、 0: Vacuum, 1: Generator, 1A: Mercury Exhaust Inspection Room, 1B: Means of increasing oxygen level, 1C: Alcohol cold heat, 1D: Fuel injection pump, 1F: Condensate pump, 1G: Heat pump, 1H: Pumping pump, 1J: Water pumping apparatus, 1Y: Combustor, 1b: Fuel, 1c: Specific substance, 1d: Mercury, 1e: Coated steel ball (coated with impact reducing means 2G) 1e: Coated mercury (spherical stainless steel durable material or impact 1g: Gravity acceleration part, 1h: Horizontal axis, 2: Sunlight heater (tilt and rotate sunlight with long lens) 2a: Water condenser, 2a: Condenser cooler, 2b: Solar thermal augmentation suspension bridge (vertically suspended lifting gear left and right to tilt and track sunlight with multiple steps of long lens) 2c: heat insulating material, 2d: long lens, 2e: water surface, 2f: lifting tool left, 2g: hanging Ingredient right, 2h: seawater cooler, z: Solar air heater, 2A: heat resistant material, 2B: heat absorbing material, 2C: compression heat recovery device, 2D: power increase means, 2E: power increase sphere (liquid metal such as liquid lead, liquid tin or liquid zinc, etc. Platinum ball, coated platinum ball, gold ball, coated gold ball, platinum alloy ball, gold alloy ball, lead alloy ball, silver alloy ball, coated platinum alloy ball, coated gold alloy ball, coated lead ball, coated silver alloy ball, tungsten alloy Balls or coated tungsten alloy balls or tungsten steel balls or coated tungsten steel balls or tantalum alloy balls or coated tantalum alloy balls or molybdenum steel balls or coated molybdenum steel balls or molybdenum cast iron balls or coated molybdenum cast iron balls or silver balls or coated silver balls etc Metal spheres and coated metal spheres) 2F: Augmented sphere lifter, 2G: Impact reduction means (coating of small spheres, lubricating oils, incombustible liquids, rubbers, plastics, etc.) 2H: cold heat condenser, 2J: Liquid metal heat exchange Converter, 2K: Lubricant material, 2X: air heat exchanger, 2Y: water heat exchanger, 2Z: mercury heat exchanger, 3: friction loss reduction means (water repellent action, heating high temperature means, coating etc. optimum utilization known Technology to reduce friction loss 3A: Water repellent action (means to reduce friction loss with water) 3B: Heating high temperature means (high temperature with existing technology such as electric resistance and electromagnetic heating) 3C: Cold heat recovery means, 3E: Impact reduction Materials (mercury, liquid metal, water) 3G: Water repellant (means for reducing friction loss with mercury) 4A: Turbine blade cross section (existing cross section) 4B: Turbine blade cross section (small output surface curve cross section) 4C: Turbine blade cross section Output surface straight section) 4D: Turbine blade cross section (output opposite surface straight section) 4E: Turbine blade cross section (output opposite curved surface minor cross section) 4F: Turbine blade cross section (existing opposite section) 4X: Turbine blade cross section (4A to 4F More choice Cross section 5C: air exhaust chamber, 6: nozzle, 6a: nozzle injection part, 6b: nozzle injection part, 6d: nozzle injection part, 6z: water injection pump, 6A: superheated steam injection nozzle, 6B: liquid lead injection pump 6C: Liquid tin injection pump, 6D: Liquid bismuth injection pump, 6E: Liquid zinc injection pump, 6F: Compressed air injection nozzle, 6H: Liquid cadmium injection pump, 6I: Liquid indium injection pump, 6J: Liquid gallium injection pump, 6K: liquid thallium injection pump, 6L: liquid metal injection pump, 6M: metal injection pump, 6X: fuel injection nozzle, 6Y: combustion gas injection nozzle, 6Z: mercury (liquid metal) injection pump, 7: fuel injection valve, 7A : Rotor 7B: Rotor 7B, 7C: Screw, 7E: Rotor arm, 8a: All rotors -Bin, 8b: All moving wing water turbine, 8c: Turbine blade, 8d: Side plate, 8e: Cylindrical cylinder, 8E: All moving wheel bounced wheel mercury turbine, 8F: All moving wheel bounced wheel Gravity turbine, 8G: All wing Covered metal sphere gravity solar thermal turbine, 8K: liquid metal gravity opposing turbine, 8K: facing in-line all moving wing impacting wheel turbine, 8L: in-line all moving wing impacting ball turbine, 10: hull, 10A: cabin, 10a: enlarged diameter compression chamber, 10b : Flight control room, 10c: Control room, 10d: Guest room, 10e: Cargo room, 11A: Bulkhead, 11B: Water room 11C: Air room, 11D: Vacuum room, 16: Crankshaft, 16A: Horizontal axis, 21: Expansion diameter Piston, 24: combustion gas control valve, 24A: compressed air control valve, 25: overheated steam control valve, 25B: high temperature water control valve, 25a: intake valve, 25b: fuel control Valve, 28a: Air, 28a: Internal air, 28a: Air tube air, 28b: Compressed air heat amount, 28A: Intake air passage, 28B: Air passage inlet, 37a: Magnetizing friction wheel, 37b: Internal magnetization friction wheel, 38a: flying body, 38b: flying wing, 38c: flying wing, 38d: vertical wing, 38e: wing leading edge, 38g: surface wing, 38h: floating surface, 38A: gravity plane, 38B: air suction jet water jet vessel , 38C: water suction jet vessel, 39A: solar thermal gravity helicopter 39C: combined engine jet part 78W solar thermal gravity plane, 39B: solar thermal gravity helicopter 39C: liquid metal gravity solar thermal plane, 39C: solar thermal gravity helicopter, 39C: liquid metal gravity solar thermal flight Ship, 39C: Metal sphere water gravity solar thermal flight vessel, 39D: Screw ship, 39D: liquid metal gravity solar thermal ship, 39F: solar thermal gravity plane, 39G: solar thermal gravity airship, 39C: flight ship, 40A: rudder, 46: magnet part, 49: combustion gas, 49B: chimney combustion gas calorie, 49C: factory Heat quantity used 50: Superheated steam 51: Air extractor 51: Combined extractor 52a: water 52b: water (water whose temperature changes with sunlight) 52b: high temperature water 52d: heat 52d: water temperature heat, 52d: Superheated steam thermal, 52e: Cold, 52e: Water-cooled heat, 52e: Compressed air cold, 52e: Alcohol cold, 52e: Ice-cooled heat, 55: Gear-type synchronizer (including magnetic friction synchronizer) 55B: Magnetic friction shift Device (including gear type and water pump combination) 55Y: Gear type transmission (selected from existing transmissions) 60A: Inner shaft device, 60 : Outer shaft device, 60C: Inner blade group, 60D: Outer blade group, 77B: Cylindrical outer box, 77D: Water jet outer box, 77F: Jet outer box, 77G: Cylindrical rotating part, 77a: Turbine outside Box 78A: united engine injection unit 78B: united engine injection unit 78K: united engine injection unit 78S: united engine injection unit 78T: united engine injection unit 78U: united engine injection unit 78V: united engine injection unit 78W: Combined engine injection part 78X: Combined engine injection part (78S78T78U78W selected) 79K: Combined engine injection part 79M: Water jet, 79S: Water jet, 79T: Water jet, 79U: Water jet (water suction jet) 79V: Water jet (selected from 79S 79T) 79X: Water jet (Water suction jet) 79Y: water jet (air suction jet) 79Z: water jet (air suction jet) 80: bearing, 80a: thrust bearing, 80A: joint, 80B: clamp, 81: spindle, 81a : Fulcrum, 84: Double reversing magnetic friction power transmission device (including gear type and water pump combined use) 84 Y: Double reversing gear device (existing technology) 94: Fixed outer box, 94A: Outer box vertical part, 95: High temperature Water reservoir, 95a: combustion gas reservoir, 95b: compressed air reservoir, 95c: superheated steam reservoir, 95A: water absorption path, 95B: fuel reservoir, 96A: water supply channel, 97: check valve, 103: cold heat recovery device,
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