JP2011185063A - Various energy conservation cycle combined engine - Google Patents
Various energy conservation cycle combined engine Download PDFInfo
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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78A太陽熱重力飛行機39A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、太陽光加熱空気を種に大気圧同速度同容積仕事率を、既存蒸気タービンの2.3万倍前後水銀等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温熱+圧縮空気28a冷熱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78A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を1200度に近付けて、真空0〜大気圧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の吸引出力を真空部飛行で最大にし、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、2.3万倍前後水銀等仕事率太陽熱タービン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78A太陽熱重力飛行機39A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. There is information that thermal energy can be obtained 3 to 10 times the power used by the heat pump with the 78A solar thermal gravity airplane 39A, and the same atmospheric pressure same speed work rate can be obtained by using solar heated air as a seed. .30,000 times mercury, etc. Power factor gravity turbine driven heat pump recovers compression heat, 3 to 10 times energy of both heat and cold are infinite recovery utilization energy preservation cycle, suction air of solar heating is suctioned and compressed The operation of heat exchange superheated steam 50 heat + compressed air 28a cold heat is carried out several times by setting the heat suction compression 1200 degree etc. as 1000 degrees etc., and the theoretical best estimate Agent superheated steam 50 + oxidant compressed air 28a Challenge the infinite production even at fuel cost 0, united engine injection part 78A injection heats the outer peripheral superheated steam 50 as the 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 are injected into the high temperature high speed combustion of two stages of fuel injection in the process of injection, the superheated steam 50 is brought close to 1200 degrees, 800 degrees of superheated steam which approaches vacuum 0 to atmospheric pressure 100 degrees Heating to a certain degree, etc., increasing the superheated steam volume, maximizing the injection propulsion output and the suction output of the combustion gas 49 in the vacuum part flight, and solving the defect of the scramjet by the increase of the combustion gas suction output; Concerning technology such as combined engine injection part 78A solar thermal gravity airplane 39A aiming at space utilization of air resistance 0CO2 exhaust 0 including 30,000 mercury power etc. solar power turbine drive
燃料費僅少の太陽熱重力飛行機39A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、竪型被覆金属球水銀重力太陽熱タービン駆動等の熱ポンプ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水銀の圧縮空気冷熱加速タービン駆動で低圧密閉空気循環とし、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78A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や外周から最適時間環状加熱して、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78A技術に関する。 Aim for zero fuel cost space use with solar thermal gravity airplane 39A etc. with minimal fuel cost. Air heated by solar light in the atmosphere is drawn with heat pump 1G such as vertical coated metal sphere mercury gravity solar heat turbine drive etc. Compressive 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 heat to combustion gas 49 cold heat and propellant The superheated steam 50 is produced, and in the space, the low pressure closed air circulation is driven by the compressed air cold heat acceleration turbine of the coated metal sphere mercury, and the superheated steam production efficiency is raised by the direct sunlight 120 degrees C and the long lens 2d and the heat pump. At the time of space rise, in the process of producing superheated steam 50 with compressed air 28a compression heat recovery device 2C, increase the amount of 24-400MPa superheated steam production by using fuel-injection combustion combustion gas 49 multiple times, united engine The combustion unit 78A supplies combustion gas to the combustor 1Y and supplies superheated steam to the outer circumference, and heats the superheated steam of the fuel injection combustion outer circumference to 24-400MPa combustion gas 49, and after the two-stage combustion or the three-stage combustion, the superheated steam The ring is heated for an optimal time from the inner week and the outer circumference, and the rocket is combined with high pressure large expansion speed of steam turbine and high speed combustion of scramjet, 10 to 100 times pressure 10 times thermal energy injection 100 to 1000 times injection output of existing jet The aim is to combine engine injection part 78A technology to shift to the experimental best engine.
竪型被覆金属球水銀重力太陽熱タービン8G駆動各種重力タービン併用等として、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太陽熱タービン駆動として、被覆金属球水銀を水銀噴射ポンプ6Zで噴射し、温熱加速や冷熱加速で太陽熱タービン駆動重力加速追加駆動して、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、被覆金属球水銀の転がり接触回転出力の増大として、竪型被覆金属球水銀重力太陽熱タービン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太陽光加熱の空気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で熱交換太陽光加熱の別空気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/秒を、既存蒸気タービンの2.3万倍前後水銀等仕事率にし、実験最良に移行の竪型被覆金属球水銀重力太陽熱タービン8G技術に関する。 Vertical type coated metal sphere Mercury gravity solar thermal turbine 8G driven Various gravity turbine combined use etc. Mercury or liquid metal (Lead alloy core 500 degree or less liquid metal alloy) as impact reduction material 3E, metal sphere (platinum sphere containing alloy) A coated metal sphere is coated on a metal sphere, such as a gold sphere, tungsten sphere, steel sphere, molybdenum sphere, cast iron sphere, silver sphere, copper sphere, nickel sphere, cobalt sphere, chromium sphere, etc. The core of the liquid metal is a lead alloy as a liquid metal at 500 degrees or less, the lead alloy is used as the core of the liquid metal, and the coated metal bulb mercury is injected by a mercury jet pump 6Z as a solar heat turbine drive that optimally corresponds to the amount of resources. Drive Gravity Acceleration Additional drive is performed to inject the turbine blade cross section 4X into the turbine blade 8c which is 2 to 26 times the size of the existing steam turbine, and increase the rolling contact rotational power of the coated metal ball mercury and The sun-shaped coated metal sphere mercury gravity solar heat turbine 8G rotation, suction air path 28A constituted by long lens 2d heat absorbing material 2B suction air 28a of solar heating, compression by heat pump to around 900 degrees, compression Heats the separate air 28a for heat exchange solar heating with the heat recovery unit 2C to around 500 ° C to make suction compression 1200 ° C, etc., and continues the heat recovery to make the compressed air 28a thermal cold-heat production infinite continuous mass, atmospheric pressure The same speed work volume kg kg m / sec. Is about 23,000 times the mercury work rate of the existing steam turbine, etc., and relates to the vertical type coated metal sphere mercury gravity solar thermal turbine 8G technology of transition best in the experiment.
3.6万倍白金球仕事率理論最良タービン等から、現状を人類絶滅狙う宇宙人の陰謀と考えると、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 aliens who aim for extinction of humanity from the 360,000 times platinum sphere work rate theory best turbine etc., the sea surface temperature rise of thermal power nuclear power generation is considered to have no effect on the environment, but the sea surface temperature If the temperature rises 7 degrees above the surrounding area, the amount of evaporation will increase explosively, abnormal weather occurrence is obvious, and mixing and dispersing with surrounding seawater will raise the temperature of the entire sea surface, so nutrients such as nitrogen, oxygen and CO2 will be accumulated on the sea surface in the winter. It is consistent with the present situation as the human food supply such as fish and seaweeds is drastically reduced by making the natural phenomenon that supplied the water impossible, and even if the sea surface temperature continues to rise 7 degrees for 100 years, it reduces CO2 emissions with nuclear power generation. As the sea surface temperature rises by 7 degrees, the area will grow 10% and exceed 1000 times, so CO2 in seawater will be released into the atmosphere, and the concentration of CO2 will be greatly increased, and flooding, heavy rain, wind speed 10 times 300m / s typhoon or South as the monsoon Close to the ice to 0, 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水銀重力太陽熱タービン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, the consumption of fuel is limited, so that it can be used as a supply facility for heat, electricity and cold heat during stoppage, as it can be used as a supply facility for heat, electricity and cold heat, 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の宇宙利用全盛の重力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0CO2排気0の重力発電蓄電池駆動の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 the resources are exhausted, the space use prime gravity airplanes with air resistance 0CO2 exhaust 0 are minimized and fossil fuel combustion is minimized, leaving limited resources in the descendants and the seawater temperature rise 0CO2 exhaust 0 gravity power storage battery Since it is impossible to cooperate as a driving vehicle or ship and can not cooperate if the profit is low, it is necessary for the world's No. 1 in the world to have excellent profit ratio, and to have a space flight cheer of zero CO2 exhaust.
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78A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 a space ascent, the combined engine injection unit 78A aims for a short time injection propulsion with 100 times the pressure of the existing jet and 10 times the amount of thermal energy injection 1000 times the injection output. 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.
竪型被覆金属球水銀重力太陽熱タービン8G駆動+各種重力タービンと併用駆動可能とし、宇宙では温熱加速と冷熱加速にして大気中では重力追加駆動で使用して、被覆金属球水銀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、竪型被覆金属球水銀重力太陽熱タービン8G駆動の各種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28Aを密閉して循環空気路とし、冷熱タービン排気を直射120度太陽光と長レンズ等で回収して、500度等に加熱して熱ポンプにより1200度前後に圧縮し、圧縮熱回収器2Cで熱交換過熱蒸気50製造にして、温熱タービンを駆動その排気を−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78V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理論最良ロケット推進にし、過熱蒸気膨張速度が真空で最大のため既存ロケット地上大量噴射は最悪と考え、既存航空機最高飛行高度付近より大出力ロケット推進して、宇宙到達燃料費を1/100以下等僅少にし、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。 Vertical-type coated metal sphere mercury gravity solar thermal turbine 8G drive + various gravity turbines can be used in conjunction with driving, in the space to use thermal acceleration and cold acceleration to make gravity additional drive in the atmosphere, coated metal sphere mercury gravity solar thermal engine rotational output In order to generate injection propulsion output 100 times pressure 10 times thermal energy injection short time 1000 times injection propulsion output of existing jet aircraft aiming at various types of gravity solar thermal engine driven by vertical coated metal sphere mercury gravity solar thermal turbine 8G, direct sunlight in space The intake air passage 28A is sealed to form a circulating air passage by utilizing the excellent environment of 120 ° C. and 150 ° C. and utilizing the excellent environment of the superheated steam turbine drive and the superheated steam production. Exhaust gas is collected by direct sunlight at 120 ° C and long lens etc., heated to 500 ° C and compressed by heat pump to around 1200 ° C, compression heat The heat exchange superheated steam 50 is produced by the collecting vessel 2C, and the thermal turbine is driven to repeat the circulation of cooling its exhaust at the -150 degree shade part to make it condensed water, and normally it is heated by the combustion gas use 0 combined engine injection part 78V Only the steam 50 is injected and the injection propulsion output is generated, and the fuel amount is 0 and the injection jet power is aimed at 10 times the injection propulsion power theory theory best rocket propulsion and the superheated steam expansion speed is maximum in vacuum and the existing rocket ground mass injection is the worst The idea is to promote high power rockets from the vicinity of the maximum flight altitude of existing aircraft, reduce the attainment fuel cost to less than 1/100, etc., and aim to achieve space utilization with various ships and aircraft of the existing world. There is an effect left to the offspring.
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の竪型被覆金属球水銀重力温熱タービン8G駆動は、増大球上昇装置2Fを設けて被覆金属球水銀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冷熱タービンの選択使用として、2種類使用は温熱タービン+冷熱タービン使用にし、被覆金属球水銀を水銀噴射ポンプ6Zで噴射して過熱蒸気温熱加速重力加速度加速して、竪型被覆金属球水銀重力温熱タービン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78Aを駆動太陽熱重力飛行機39A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 sphere mercury gravity thermal turbine 8G drive of FIG. 1 is provided with an increase sphere raising device 2F to ascend and store the coated metal sphere mercury at the top, and vertically 1 to 10 stages etc. turbine in the outer box 77a The multistage is used in multiple stages, and it is used according to the use, and one kind of use is used as the selective use of thermal turbine 8G cold heat turbine, two kinds use is used as thermal turbine + cold heat turbine, coated metal sphere mercury is injected by mercury jet pump 6Z Then, the superheated steam thermal acceleration gravitational acceleration is accelerated to drive the vertical coated metal ball mercury gravity thermal turbine 8G, the horizontal axis 1h is provided between the turbines, and the generator 1 or the heat pump 1G The compression heat recovery unit 2C, the water heat exchanger 2Y, and the air heat exchanger 2X are driven to alternate the rotational direction of the turbine 8G to offset the vibration and noise slightly, and the heat pump 1G and the compression heat circuit using solar heat as a seed To produce almost infinite heat (superheated steam of compressed air heat) and cold heat (compressed air mass) with the 2C, for example, around 500 degrees 24 to 400MPa superheated steam thermal + 100 to around 200 degrees 24 to 400MPa compressed air cold Divide and save, drive the thermal turbine + cold heat turbine with a part and gravity, drive the combined engine injection part 78A at most part to the solar thermal gravity plane 39A flight, and use it for supply of heat and electricity during stop .
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水銀を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で吸入圧縮して、最適圧力冷熱にし、合体機関噴射部78Aの最適圧力高速冷熱で吸引して、混合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で吸入圧縮して、合体機関噴射部78Aの最適圧力高速温熱で吸引し、混合合流推進剤で使用する循環にして、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、被覆金属球水銀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/秒を、既存蒸気タービンの2.3万倍前後水銀仕事率等にし、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、熱ポンプ駆動して圧縮空気冷熱製造と温熱(過熱蒸気)を製造する、竪型被覆金属球水銀重力温熱タービン8Gにします。 In the process of thermal turbine 8G drive, the coated metal sphere mercury cooled by cold heat turbine 8G is heated by heating temperature around 500 degrees by heating steam 50 to increase the cold heat turbine drive compressed air cold heat volume to increase rotational power, cold heat turbine The exhaust is sucked and compressed by the combined extractor 51 to obtain optimum pressure cold heat, and is sucked by the optimum pressure high-speed cold of the united engine injection part 78A to be used as a mixed and combined oxidant circulation, and the superheated steam of the thermal turbine exhaust is also joined The suction and compression by the extractor 51, suction with the optimum pressure high-speed heat of the united engine injection unit 78A, and the circulation used by the mixing and merging propellant, the inner moving blade group 60C and the outer moving blade group 60D are hydraulics that support a large weight Equipped with levitation additional thrust bearing 80a, and can be fully automatically machined so that each stage has the same diameter and substantially the same shape, and can be assembled into a multistage blade group and a multistage turbine, as well as assembly is easy. The gravity acceleration part 1g which accelerates the coated metal sphere mercury is equipped with a horizontal axis 1h and a through hole, and the generator 1, heat pump 1G, etc. are driven outside the turbine outer box 77a, and the air of solar heating is heated. The compression temperature is around 1000 degrees, another air of solar heat heating is heated to 600 degrees C etc by air heat exchanger 2X, compression is around 1200 degrees, and heat production of high pressure compressed air 28a cold heat and superheated steam 50 heat repeatedly. Increase the volume and make the same atmospheric pressure same volume work volume kg weight m / s 23,000 times that of the existing steam turbine, etc., 2 to 26 times the cross section of the existing turbine blade cross section Vertical-type coated metal sphere mercury that jets onto the turbine blade cross section 4X and makes maximum use of gravity and solar heat by rolling contact rotational power generation and heat pump drive to produce compressed air cold heat and heat (superheated steam) Gravity thermal turbine 8G.
図2の竪型被覆金属球水銀重力冷熱タービン8G駆動も、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水銀を増大球上昇装置2Fで最上部に上昇保存し、被覆金属球水銀を水銀噴射ポンプ6Zで噴射して圧縮空気28a冷熱加速重力加速度加速して、竪型被覆金属球水銀重力冷熱タービン8Gを被覆金属球水銀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水銀で加熱して、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水銀を冷却し、冷却した被覆金属球水銀で温熱タービン8G駆動被覆金属球水銀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空気28aを合流抽出器51で吸入圧縮し、低圧冷熱排気として出力増大にして、合体機関噴射部78Aの最適圧力高速冷熱で吸引し、混合合流酸化剤で使用する循環にして、熱ポンプと共に被覆金属球水銀重力冷熱タービンによる噴射推進出力の上昇にし、圧縮空気28a冷熱の最大限活用にします。 The vertical coated metal sphere mercury gravity cold heat turbine 8G drive of FIG. 2 is also provided with 1 to 10 stages etc. of turbine vertically in multistage vertically in the outer box 77a to use the number according to the application, temperature rise by thermal turbine drive The coated metal sphere mercury is elevated and stored at the top with the increase sphere lifter 2F, and the coated metal sphere mercury is jetted by the mercury jet pump 6Z and compressed air 28a cold thermal acceleration Gravity acceleration is accelerated, the wedge type coated metal sphere mercury gravity The cold heat turbine 8G is driven by the rolling contact of the coated metal sphere mercury, and the compressed air 28a which approaches absolute 0 degrees in the process of driving is heated by the coated metal sphere mercury whose temperature is increased to increase the compressed air volume velocity and the turbine output The temperature is increased by cooling the coated metal bulb mercury, and the cooled coated metal bulb mercury is combined with the heated turbine 8G driven coated metal bulb mercury temperature to increase the temperature of the cooled thermal turbine exhaust air 28a. The suction pressure is compressed by the extractor 51, the output is increased as low pressure cold exhaust, the optimum pressure high speed cold of the united engine injection section 78A is sucked, and the circulation is used with the mixing joint oxidizing agent and the heat pump coated metal sphere mercury gravity Increase the injection propulsion output by the cold heat turbine, and make the best use of the compressed air 28a cold.
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冷熱で被覆金属球水銀を加速駆動する、竪型被覆金属球水銀重力冷熱タービン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/秒を、既存蒸気タービンの2.3万倍前後水銀仕事率等にし、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とし、重力や太陽熱を最大限利用する、竪型被覆金属球水銀重力冷熱タービン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 separately, use compressed air 28a cold heat accelerates coating metal ball mercury acceleration, vertical type coating metal sphere mercury gravity cold heat turbine 8G, inner rotor blade group 60C outer rotor blade group 60D has a hydraulic levitation additional thrust bearing 80a to support a large weight to enable multi-stage turbine, compress solar heating air to around 1000 degrees, and separate solar heating with air heat exchanger 2X At 500 ° C., etc. and compression to around 1200 ° C., and repeatedly to increase the production volume of high pressure compressed air 28 a and superheated steam 50 at atmospheric pressure same speed same volume work rate kg weight m / m Make the rolling contact rotational power generation by injecting it to the turbine blade cross section 4X which is about 23,000 times the mercury work rate of the existing steam turbine, etc. and 2 to 26 times the cross section of the existing turbine blade. And to make the best use of solar heat, we will make a vertical coated metal sphere mercury gravity cold heat turbine 8G.
図3の合体機関噴射部78A太陽熱重力飛行機39A噴射推進出力発生では、重力使用が限定されるため飛行胴38a垂直翼38dを一体として、複数竪型被覆金属球水銀重力タービン8G台数選択使用で落差を最適にし、翼前縁心38e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、複数タービン駆動の熱ポンプ1Gで圧縮1000度前後にし、空気熱交換器2Xの太陽熱加熱別空気28aで熱回収、熱ポンプ1Gで圧縮熱回収を繰り返す熱製造として、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、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温熱と燃焼ガス49冷熱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78Aに供給し、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、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る、各種太陽熱重力飛行機39A類や各種航空機類で燃料費0に近い宇宙利用全盛にし、大気中を通常飛行時には既存ジェット機の10〜100倍圧力1/10熱量過熱蒸気50噴射等として、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、既存宇宙ロケット地上大量噴射を最悪噴射と考え、既存航空機最高飛行高度付近より大出力ロケット推進して、宇宙到達燃料費を1/100以下等僅少にします。 In the combined engine injection part 78A solar thermal gravity airplane 39A injection propulsion power generation of FIG. 3, since the use of gravity is limited, the flight cylinder 38a vertical wing 38d is integrated, and a drop occurs by using a plurality of types of coated metal sphere mercury gravity turbine 8G In the process of suctioning the air 28a from the blade leading edge 38e air suction port 28B, the solar heating air 28a is sucked by the suction air passage 28A composed of the long lens 2d heat absorbing material 2B to drive multiple turbines. The heat pump 1G makes the compression around 1000 degrees, the solar heat of the air heat exchanger 2X recovers heat with the separate air 28a, and the heat pump 1G repeats the compression heat recovery as heat production. As long as combustion is performed, high-pressure combustion, heat exchange, cooling, combustion, repeated compression at 1200 degrees, etc., heat recovery is repeated with the water heat exchanger 2Y, and the overheated steam 50 temperature heat and combustion 49 cold heat is supplied to the united engine injection section 78A at a pressure 10 to 100 times the existing jet injection pressure, etc., and the superheated steam 50 around the fuel injection combustion is heated 10 times by a total amount of heat, etc. Close to 100% of existing jets for a short time, and approach to the supersonic Mach 32 Earth escape velocity and speed of light in space. During normal flight, compressed air 28a oxidizer cold heat and superheated steam 50 propellant thermal storage are increased as normal flight 10 to 100 times pressure 1/10 calorific superheated steam injection of the existing jet aircraft, and existing space rocket ground mass injection We think that it is the worst injection, and promote the high power rocket from near the maximum flight altitude of the existing aircraft, and make the cost to reach space fuel as small as 1/100 or less.
大気中を飛行時には複数の竪型被覆金属球水銀重力タービン8G横軸1h駆動の、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、横並び又は前後並びとして、用途に合わせた台数を夫々1〜10段に設けて、用途に合わせて落差を増大した出力増大とし、被覆金属球水銀を水銀噴射ポンプ6Zで噴射して、分割保存した圧縮空気熱量や圧縮空気冷熱で加速重力追加加速し、夫々の竪型被覆金属球水銀重力タービン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/秒を、既存蒸気タービンの2.3万倍前後水銀仕事率等にし、熱ポンプ多数を駆動して、24〜400MPa過熱蒸気50温熱+24〜400MPa圧縮空気28a冷熱を限り無く増大し、空気吸引噴射する噴射推進出力の発生は、合体機関噴射部78Aに供給した、過熱蒸気推進剤+圧縮空気酸化剤に燃料噴射燃焼双方の最大速度噴射等として、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、合体機関噴射部78A円筒回転部77G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、宇宙利用やビルの屋上や月面等何処でも飛行場として着陸可能にします。 When flying in the atmosphere, heat pumps 1G, compression heat recovery devices 2C, air heat exchangers 2X, and water heat exchangers 2Y driven by a plurality of vertical-coated metal spheres mercury gravity turbine 8G horizontal axis 1h are arranged side by side or side by side, The number according to the application is provided in 1 to 10 stages respectively, and the power increase with an increase in the head according to the application is made, and the coated metal sphere mercury is injected by the mercury injection pump 6Z, and the compressed thermal energy and compressed air divided and stored Cold energy accelerated Gravity Additional acceleration is carried out and injected into each vertical-type coated metal sphere mercury gravity turbine 8G to make the turbine blade cross section 4X 2 to 26 times of the existing steam turbine, and to the turbine blade 8c by injection rolling contact drive gravity or Make maximum use of sunlight, make atmospheric pressure same velocity same volume work power kg heavy m / sec 23,000 times of existing steam turbine and so on mercury work ratio etc, drive heat pump many, 24- Over 400MPa Steam 50 temperature +24-400MPa compressed air 28a cold heat is increased without limit, and the generation of the injection propulsion output which carries out air suction injection is both the fuel injection combustion to the superheated steam propellant + compressed air oxidant supplied to the combined engine injection part 78A 10-100 times pressure 1/10 injection heat 10 times injection promotion output enlargement etc. of the existing jet machine as maximum speed injection etc., united engine injection part 78A cylindrical rotation part 77G is rotated 180 degrees or more, reverse injection Vertical Ascent Allows vertical descent, and allows landing as an airfield anywhere on the roof or on the moon, in space use, and on buildings.
宇宙到達時には竪型被覆金属球水銀重力タービン8G駆動の過程で、空気路入口28Bを密閉した空気路28Aとし、120度前後直射太陽光の熱量を長レンズ2d熱吸収材2Bで500〜800度等空気28aとして、熱ポンプ1Gで吸入圧縮1200度前後にして熱回収過熱蒸気推進剤を増大し、冷熱タービン8Gを駆動して空気28a温度圧力を低下して、長レンズ2d熱吸収材2Bで500〜800度空気28a温度とし、熱ポンプ1Gを駆動圧縮1200度等として熱回収過熱蒸気推進剤製造を繰り返して、過熱蒸気推進剤を限り無く増大し、宇宙では過熱蒸気50を最も効率良く製造貯蔵する熱ポンプ1Gや太陽光加熱にして、宇宙での噴射推進は過熱蒸気50による噴射推進とし、宇宙での圧縮空気28aは過熱蒸気50の製造に使用して、タービン8Gで多数の熱ポンプ1G駆動と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78A酸化剤の最適圧力部に高速吸引合流し、燃料噴射着火燃焼噴射推進出力の増大に使用します。 At the time of space arrival, in the process of driving the bowl-shaped coated metal sphere mercury gravity turbine 8G, the air passage inlet 28B is made the air passage 28A sealed, and the heat quantity of direct sunlight around 120 degrees 500 to 800 degrees As the equal air 28a, increase the heat recovery superheated steam propellant at around 1200 ° C with suction and compression with the heat pump 1G, drive the cold heat turbine 8G to lower the temperature pressure of the air 28a, and use the long lens 2d heat absorbing material 2B The heat recovery superheated steam propellant production is repeated by setting the temperature of 500 to 800 degree air 28a, heat pump 1G drive 1200 degree compression etc, and superheated steam propellant is increased without limit, and superheated steam 50 is produced most efficiently in space For the heat pump 1G to store and solar heating, the injection and propulsion in space is by the superheated steam 50 and the compressed air 28a in space is made of the superheated steam 50 Used in the turbine 8G to enable long-distance space travel as multiple heat pump 1G drives, and in heat return to compressed air 28a, making it possible to carry out suction compression heat exchange of high pressure high temperature air 28a including frictional heat upon earth return. The cold heat turbine 8G is driven at this time, and the exhaust is compressed to the suction optimum pressure by the joint extraction unit 51, and is joined at high speed to the optimum pressure unit of the combined engine injection unit 78A oxidant to increase the fuel injection ignition combustion injection propulsion output Used for
図4の合体機関噴射部78A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、圧縮熱回収器2C圧縮空気28aに燃料噴射燃焼熱交換過熱蒸気製造して、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内部環状に具備して、複数1段噴射燃焼流の燃料噴射ノズル6Xより燃料噴射2段燃焼器複数最適距離環状燃焼にし、過熱蒸気50を外周と内周より加熱噴射出力と燃焼ガス吸引出力を増大して、燃焼ガス燃焼流に複数の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、必要に応じて同様に4段燃焼し、過熱蒸気50噴射流を内周と外周から環状加熱して、大気圧100度宇宙0度に近付く過熱蒸気を500度等とし、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 78A 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. In the process of producing the superheated steam 50, the fuel injection combustion heat exchange superheated steam is produced in the compression heat recovery unit 2C compressed air 28a, and the heat is recovered multiple times by multiple compression fuel injection combustion, and the high pressure combustion gas 49 oxidizing agent with unlimited The superheated steam 50 propellant is increased as much as possible without storage, the combustion gas control valve 24 is opened at the ascension of space, and the combustion gas 49 around 200 degrees C. to 400 MPa is supplied to the uppermost stream of the combustion gas reservoir 95a combustor 1Y, Fuel 1b is injected from the fuel injection nozzle 6X by the fuel control valve 25b open fuel injection pump 1D, and the overheated steam 50 of the ignition combustion outer periphery is heated to the combustion combustion temperature rise in the combustor 1Y uppermost stream. The injection output of both heating is increased by heating the steam reservoir 95c at around 400 degrees and around 24 to 400 MPa superheated steam 50, and the multiple combustion gas injection nozzles 6Y of the combustor 1Y are provided in an annular shape inside the superheated steam reservoir 95c to perform multiple one-stage injection combustion The fuel injection two-stage combustor multiple optimal distance annular combustion from the fuel injection nozzle 6X of the flow, the heating injection output and the combustion gas suction output are increased from the outer circumference and the inner circumference of the superheated steam 50, and a plurality of combustions in the combustion gas combustion flow The gas injection nozzle 6Y is provided, and the fuel injection three-stage combustor multiple optimal distance from each fuel injection nozzle 6X is annular combustion, and if necessary, four stages of combustion are similarly performed, and the superheated steam 50 injection flow is From annular heating, superheated steam approaching atmospheric pressure 100 degrees and space 0 degrees is set to 500 degrees, etc., and cheap jet output of 10 to 100 times pressure and 10 times mass injection of existing jets is aimed.
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78A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とロケット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78Aを駆動し、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+ロケットと合体して、過熱蒸気50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 78A that makes the best combination by utilizing the respective advantages, existing scramjet high speed combustion and steam turbine The high-pressure injection and the rocket are combined into a high-temperature and high-pressure injection, and the combustion of the compression heat recovery device 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 sunlight heating air 28a is produced as a compressed oxidant, compressed to 1000 ° C., etc. and compressed into a heat recovery unit 2C to produce a propellant for heat exchange superheated steam 50. In order to prevent global warming, in which one-stage combustion, two-stage combustion, and three-stage combustion become minimal, the superheated steam 50 approaching 100 degrees is heated to 500 degrees etc. Increase the majority of the heat steam volume Increase the injection speed Increase the suction force of the combustion gas 49 to drive the combined engine injection part 78A that mixes and injects the superheated steam 50 and the combustion gas 49 most efficiently, scramjet high speed combustion + High-pressure injection large expansion speed of steam turbine + Combined with rocket, store and use oxidant and propellant of superheated steam 50 and compressed air 28a, make cylinder rotation part 77 G rotate more than 180 degrees, vertically rise and vertical It enables descent and reverse injection, makes airfields and space use prime everywhere, and makes day trips etc. possible anywhere on earth.
理論最良タービンの竪型被覆金属球水銀重力太陽熱タービン8G+各種重力太陽熱タービン選択併用を可能として、太陽光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78A太陽熱重力飛行機39A駆動として、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。 Theoretic best turbine Vertical-type coated metal sphere mercury gravity solar heat turbine 8G + various gravity solar heat turbine selection combined use, air of solar heating is suctioned, compressed and heat recovered by heat pump and stored and used with heat + cold such as 24 to 400MPa As a turbine drive combined engine injection unit 78A solar thermal gravity airplane 39A drive, vertical rise, vertical descent and reverse injection are possible, and it is possible to make airfields and space use prime everywhere, and make day trip etc. possible anywhere on earth There is a sex.
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:竪型全動翼金属球重力太陽熱タービン、 8K:被覆金属球水銀重力対向タービン、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:太陽熱重力飛行機、 39B:太陽熱重力回転飛行機、 39C:太陽熱重力ヘリコプター、 39D:スクリュー船舶、 39G:太陽熱重力飛行船舶、 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(78S78T78U78V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 Metal ball gravity solar thermal turbine, 8K: coated metal ball mercury gravity opposing turbine, 8K: facing in-line all moving wing impacting wheel turbine, 8L: in-line all moving wing impacting wheel turbine, 10: hull, 10A: cabin, 10a: enlarged diameter compression chamber, 10b: cockpit, 10c: control room, 10d: cabin, 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 car, 37b: Internal magnetization friction car , 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 Ship, 38C: water suction jet vessel, 39A: solar thermal gravity plane, 39B: solar thermal gravity rotary plane, 39C: solar thermal gravity helicopter, 39D: screw ship, 39G: solar thermal gravity airship, 40A: rudder, 46: magnetic part, 49 : Combustion gas, 49B: Chimney combustion gas heat quantity, 49C: Factory use heat quantity, 50: Superheated steam, 51: Empty Extractor, 51: Joint extractor, 52a: Water, 52b: Water (water whose temperature changes due to sunlight) 52b: High temperature water, 52d: Thermal, 52d: Water temperature heat, 52d: Superheated steam thermal, 52e: Cold energy, 52e : Water-cooled heat, 52e: Compressed-air cold energy, 52e: Alcohol-cooled heat, 52e: Ice-cooled heat, 55: Gear-type synchronizer (including magnetic friction synchronizer) 55B: Magnetic friction transmission (including gear-type and water pump) 55Y: Gear transmission (selected from existing transmissions) 60A: inner shaft device, 60B: outer shaft device, 60C: inner blade group, 60D: outer blade group, 77B: cylindrical outer box, 77D: water jet Outer box, 77F: injection part outer box, 77G: cylindrical rotation part, 77a: turbine outer box, 78A: combined engine injection part, 78B: combined engine injection part, 78K: Body engine injection unit 78S: Combined engine injection unit 78T: Combined engine injection unit 78U: Combined engine injection unit 78V: Combined engine injection unit 78W: Combined engine injection unit 78X: Combined engine injection unit (78S78T78U78V selected ) 79K: coalesced engine injection unit, 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 ( 84Y: Double reversing gear unit (existing technology) 94: Fixed outer box, 94A: Vertical part of outer box, 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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