JP2013104319A - Various energy conservation cycle combined engine - Google Patents

Various energy conservation cycle combined engine Download PDF

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JP2013104319A
JP2013104319A JP2011247018A JP2011247018A JP2013104319A JP 2013104319 A JP2013104319 A JP 2013104319A JP 2011247018 A JP2011247018 A JP 2011247018A JP 2011247018 A JP2011247018 A JP 2011247018A JP 2013104319 A JP2013104319 A JP 2013104319A
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oxygen
electricity
superheated steam
coalescence
combustion
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Hiroyasu Tanigawa
浩保 谷川
Kazunaga Tanigawa
和永 谷川
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Abstract

PROBLEM TO BE SOLVED: To solve the following problems: existing steam turbine generation reduces 1/10 of a vapor velocity by comprising half of stator blades with no power and intercepting the vapor velocity, and is akin to zero output generation, for example, in which a volume is equivalent to 43,000 times the volume of maximum speed section water.SOLUTION: The amount of electric power generation is improved to 1/10 or less by comprising half the stator blades with no power to intercept a lightweight vapor speed and the like and performing light load generation. For example, mercury gravity acceleration generation in a vacuum of 30 mmHg, in which all moving blades are double-inverted by a gear with a horizontal shaft 1h, is adopted; 100 sets of mercury injection turbines at a speed of about mach three are stacked; the amount of electric power generation per turbine is 1,355 times larger than the amount of electric power generation of the existing turbine; and a bearing load is planned to be zero. Electricity+liquid air+superheated-vapor thermal supply equipment 3D, which has been thermally-produced by a solar heater that is inexpensive and electrically-driven in such a manner that a fuel cost is set to be zero and that a power generation cost is reduced to 1/100, is employed. An automobile, a ship, an airplane and the like are driven by compressing liquid oxygen so that volume compression power can be set to be 21/60,000 of volume compression power of air compression. The fuel cost is reduced to 1/10, and the speed is made to be ten times higher. The space arrival cost of the airplane is planned to be reduced to 1/500,000. Consequently, a person can make a day trip to any place on the earth. The operational profit ratios of operations of all products are set exceptionally high and eternally kept at the highest level in the world.

Description

本発明真空中重力加速度超高速対応内外夫々円筒軸装置に環状タービン翼群嵌合の、竪型全動翼比重大物質重力タービン8N発電は、反発永久磁石9B+吸引永久磁石9Cで軸受荷重を0に近付け、歯車外周多極着磁した二重反転磁気装置85+横軸1hで次々に反転して、振動低減落差800mに100台等で発電機発電する、既存揚水発電に地球最大未利用再生可能エネルギの、真空度上昇中の重力加速度追加+音速等噴射追加+タービン数無制限落差無制限追加して、例えばマッハ3水噴射のウォータージェット加工水速度に近付けた水銀噴射速度や、落差500〜800mにタービン100台既存揚水発電の10000倍発電量狙いにし、ボイラや原子炉全廃の燃料費0各種実験が必要な発電として、重力タービン8N発電電気駆動1〜複数段熱ポンプ1Gや太陽光加熱器21とし、太陽光加熱の空気を圧縮高温として、1〜複数段圧縮熱回収器2Cで熱回収分割保存する熱製造にし、24〜200MPa過熱蒸気50温熱+液体空気28a冷熱に分割保存して、電気+液体空気冷熱+過熱蒸気温熱供給設備3D無限用途対応とし、例えば船舶や車両や飛行機等は液体酸素て受給して、圧縮容積仕事率を空気圧縮の1/600×21/100=21/60000容積仕事率にし、液体酸素や水の圧縮圧力20倍等を容易として、理論膨張機関3P回転力駆動や、酸素合体空気噴射部88Aや酸素合体水噴射部88Kの合体噴射推進にし、船舶の合体噴射推進では自然現象高速化2a海水に窒素や酸素やCO2を供給微生物や海草類増大して、食物連鎖等で魚類等人類の食料を大増大し、飛行機や自動車駆動ではCO2排気1/10や燃料費1/10や1/50万経費宇宙到達狙い等、飛行機や船舶は10倍速度狙い等、各種エネルギ保存サイクル合体機関や各種エネルギ保存合体方法の技術に関する。 The present invention is a vertical all-blade ratio critical material gravity turbine 8N power generation, in which an annular turbine blade group is fitted to a cylindrical shaft device corresponding to gravity acceleration and ultrahigh speed in vacuum, and the bearing load is reduced to 0 by a repulsive permanent magnet 9B + attractive permanent magnet 9C. Near the gear wheel, the gears are reversed one after the other by the magnetic reversal magnetic device 85 and the horizontal axis 1h, and the generator generates power at 100 vibration reduction heads of 800m. Gravity acceleration during vacuum increase + injection of sonic velocity, etc. + number of turbines unlimited head drop unlimited addition, for example, mercury jet speed close to the water jet processing water speed of Mach 3 water jet, head drop 500-800m Gravity turbine 8N power generation electric drive as a power generation that requires experimentation of fuel cost of boilers and nuclear reactors abolished, aiming to generate electricity 10,000 times that of 100 existing turbines -Multistage heat pump 1G and solar heater 21; solar heating air as compressed high temperature, heat production divided and stored in 1 to multistage compressed heat recovery unit 2C, 24-200MPa superheated steam 50 heat + Liquid air 28a divided into cold heat and stored in electricity + liquid air cold heat + superheated steam heat supply equipment 3D endless use, for example, ships, vehicles, airplanes etc. receive liquid oxygen and compressive volume work rate is compressed by air 1/600 × 21/100 = 21/60000 volumetric power, and easy compression of liquid oxygen or water with a compression pressure of 20 times, the theoretical expansion engine 3P rotational force drive, oxygen combined air injection unit 88A and oxygen combined water In the combined injection propulsion of the injection unit 88K, in the combined injection propulsion of the ship, natural phenomenon speeding up 2a Nitrogen, oxygen and CO2 are supplied to seawater. Microorganisms and seaweeds are increased, and food such as fish is consumed in the food chain. The number of energy conservation cycle coalescing engines and various energy sources such as 1/10 CO2 exhaust, 1 / 10th fuel cost and 1 / 500,000 cost space target for airplanes and automobiles, 10x speed for airplanes and ships, etc. It is related with the technique of a preservation | save coalescence method.

既存世界最多の自動車駆動往復機関は空気圧縮で膨大な燃料消費しており、竪型全動翼比重大物質重力タービン8N真空中比重大物質重力加速度発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとして供給、例えば過熱蒸気は永久凍土地下や海底のメタンハイドレートに注入、メタンと高温水に分割メタンは液体窒素冷却液体メタンで回収として、液体酸素室5Kに液体酸素5Kを受給し、液体酸素5Kの圧縮にして、圧縮容積仕事率を空気圧縮の21/60000容積仕事率にして24〜200MPa超高圧圧縮噴射にし、液体酸素5K+液体燃料1b+水52aを超高圧に圧縮理論燃焼室4Y内周等で加熱して、超高温や最適温度に加熱して理論燃焼室4Yに夫々を噴射する過程で燃料噴射燃焼し、例えばアセチレン酸素バーナー複数中心付近燃焼で外周付近高圧高温過熱蒸気50を加熱して、酸素アセチレン炎3000℃以上水の熱分解狙い酸素水素増大燃焼の各種研究にし、理論燃焼室4Yで超高圧の燃焼ガス49+過熱蒸気50として、高圧高温燃焼ガス制御弁5a開放や燃焼ガス噴射ノズル6Yより噴射し、理論膨張機関3Pを駆動して、自動車や耕耘機等各種車両類やプロペラ7Aや回転翼7Bやスクリュウ7Cを駆動し、各種車両類やプロペラ飛行機やスクリュウ船舶を駆動して、燃料費0発電電気製造の液体酸素5K使用により燃料費1/10や10倍速度狙いとし、利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。 The world's largest automobile-driven reciprocating engine consumes enormous amount of fuel due to air compression, and the vertical type moving blade specific material gravity turbine 8N vacuum specific material gravity acceleration power generation of electricity + liquid air cold heat + superheat Supply as steam heat supply equipment 3D, for example, superheated steam is injected into methane hydrate under permafrost land or underwater, methane is divided into high temperature water and methane is recovered with liquid nitrogen cooled liquid methane, liquid oxygen chamber 5K is supplied with liquid oxygen 5K Received, compressed to liquid oxygen 5K, compressed volume work rate to 21/60000 volume work of air compression to 24-200MPa ultra high pressure compression injection, liquid oxygen 5K + liquid fuel 1b + water 52a to ultra high pressure compression theory Fuel is injected and burned in the process of heating at the inner periphery of the combustion chamber 4Y, etc., and injecting each into the theoretical combustion chamber 4Y by heating to an ultra-high temperature or optimum temperature, for example, acetylenic acid High-temperature high-temperature superheated steam 50 near the outer periphery is heated by burning near the center of the burner, and the oxygen acetylene flame 3000 ° C. or more is used for various researches on oxygen-hydrogen-enhanced combustion aimed at thermal decomposition of water. The steam 50 is injected from the high-pressure and high-temperature combustion gas control valve 5a and the combustion gas injection nozzle 6Y, and the theoretical expansion engine 3P is driven to drive various vehicles such as automobiles and tillers, propellers 7A, rotor blades 7B, and screws 7C. Driving, driving various vehicles, propeller airplanes and screw ships, aiming at fuel cost 1/10 or 10 times speed by using liquid oxygen 5K for power generation electricity production, various energy aiming at the world's best profit rate The present invention relates to a storage cycle coalescence engine and a coalescence technique.

既存ジェット機ガスタービンも空気圧縮で膨大な燃料消費して、回転出力や噴射推進出力を僅少とし、空気抵抗01日に地球を16周等宇宙飛行が不可能なため、宇宙ロケットとジェットを合体した液体圧縮の酸素合体空気噴射部88A噴射推進狙いとして、竪型全動翼比重大物質重力タービン8N発電電気駆動多数の1〜複数段二重反転圧縮機3T等熱ポンプ1G+太陽光加熱器21熱製造により、24〜200MPaの過熱蒸気温熱50+液体空気冷熱28aに分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとして、飛行機の噴射推進は液体酸素5K+液体燃料1b+水52aで受給し、液体酸素圧縮により圧縮容積仕事率を空気圧縮の21/60000容積仕事率超高圧圧縮して、液体酸素制御弁5T+水制御弁5Q+液体燃料制御弁1Kを開放、夫々を酸素合体空気噴射部88A内周や理論燃焼室4Y内周等で加熱して最適温度にし、燃料制御弁25b+酸素制御弁24D+過熱蒸気制御弁25を開放して、夫々を1以上の理論燃焼室4Yに噴射燃焼して過熱蒸気熱分解燃焼等に挑戦し、例えばアセチレン酸素バーナー複数中央燃焼3300℃以上で熱分解電気分解狙いとして、過熱蒸気燃焼狙い+過熱蒸気による理論燃焼室4Yの保護燃焼+燃焼量増大噴射出力増大とし、同様に燃焼流複数段理論燃焼室4Y燃焼や吸引空気流複数理論燃焼室4Y燃焼噴射推進にして、燃焼ガス49や過熱蒸気50を24〜200MPa噴射前方の空気を吸引噴射し、宇宙到達費用を既存の1/50万狙いにして、燃料費0に近い宇宙飛行で1日に地球を16周する等地球上何処でも日帰り旅行を可能にし、各種宇宙往還飛行機類で利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。   The existing jet gas turbine also consumes a large amount of fuel due to air compression, and the rotation output and injection propulsion output are reduced, and space flight such as 16 laps on the earth is impossible on the day of air resistance. Liquid compression oxygen coalesced air injection unit 88A injection propulsion, vertical all-blade ratio critical material gravity turbine 8N power generation electric drive many 1 to multiple stage counter rotating compressor 3T isothermal pump 1G + solar heater 21 heat It is divided and stored as superheated steam temperature 50 + liquid air cold heat 28a of 24 to 200 MPa by manufacture, and the jet propulsion of the airplane is received as liquid oxygen 5K + liquid fuel 1b + water 52a as electricity + liquid air cold heat + superheated steam temperature supply equipment 3D. Compressed volumetric power by liquid oxygen compression is 21/60000 volumetric power ultra-high pressure compression of air compression, liquid oxygen control valve 5T + water control valve 5Q + The body fuel control valve 1K is opened, and each is heated to the optimum temperature by the inner periphery of the oxygen coalesced air injection section 88A, the inner periphery of the theoretical combustion chamber 4Y, etc., and the fuel control valve 25b + oxygen control valve 24D + superheated steam control valve 25 is opened. Then, each one is injected and burned into one or more theoretical combustion chambers 4Y to challenge superheated steam pyrolysis combustion, for example, acetylene oxygen burner multi-center combustion at 3300 ° C or more, aiming at pyrolysis electrolysis, aiming at superheated steam combustion + superheat The combustion of the theoretical combustion chamber 4Y by steam is increased and the combustion output is increased. Similarly, the combustion flow multistage theoretical combustion chamber 4Y combustion and the intake air flow multitheoretical combustion chamber 4Y combustion injection propulsion are set to the combustion gas 49 and superheated steam. 50 to 24 to 200 MPa Injecting the air in front, aiming for space arrival cost of 1 / 500,000, and making 16 orbits of the earth a day in space flight close to zero fuel cost Anywhere to allow a day trip, aimed at profit margins preeminent world in a variety of space shuttle airplane class, relates to a technology of various energy conservation cycle combined institutions and coalescence method.

既存船舶も空気圧縮で膨大な燃料消費して回転出力や噴射推進出力を僅少とし、低速移動に膨大な燃料を消費しているため改良し、液体酸素圧縮で圧縮容積仕事率を空気圧縮の21/60000容積仕事率にして、液体空気製造の空気圧縮機も理論最良の二重反転圧縮機3T使用追加とし、竪型全動翼比重大物質重力タービン8N発電電気駆動1〜複数段二重反転圧縮機3T等熱ポンプ1G圧縮として、太陽光加熱器21太陽光加熱の空気を圧縮高温とし、1〜複数段圧縮熱回収器2Cで熱回収分割保存する熱製造にして、24〜200MPa過熱蒸気50温熱+液体空気28a冷熱に分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとして、液体酸素5K+液体燃料1c+水52aを受給ポンプ圧縮50〜200MPaとし、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放して、酸素合体水噴射部88K内周や理論燃焼室4Y内周で夫々最適温度に加熱し、酸素合体水噴射部88Kや理論膨張機関3Pに噴射夫々を水噴射駆動や回転駆動して、酸素合体水噴射部88Kの噴射推進や理論膨張機関3Pのスクリュウ7C回転推進にし、既存船舶速度の10倍速度や1/10燃料費狙いとして、スクリュウ推進排気の過程では簡単ウォータージェット推進選択可能とし、噴射推進の過程で自然現象高速化して海中に酸素や窒素やCO2等を供給して、微生物や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、利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。   The existing ship consumes a large amount of fuel by air compression, reduces the rotational output and injection propulsion output, and consumes a large amount of fuel for low-speed movement. / 60000 volumetric power, air compressor for liquid air production is also added to use the best counter-rotating compressor 3T, vertical type moving blade ratio critical material gravity turbine 8N power generation electric drive 1-multiple stage double reversal 24G to 200MPa superheated steam by heat production by storing the heat recovered by splitting and storing the heat of the solar heating device 21 solar heating air into the compressed high temperature and the 1 to multi-stage compression heat recovery device 2C as the heat pump 1G compression of the compressor 3T etc. 50 warm heat + liquid air 28a cold and stored separately, electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D, liquid oxygen 5K + liquid fuel 1c + water 52a is a receiving pump compression 50-200MPa, The body oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened and heated to the optimum temperature in the inner periphery of the oxygen combined water injection unit 88K and the inner periphery of the theoretical combustion chamber 4Y, respectively. Each of the injections is driven into the expansion engine 3P or driven to rotate, and the oxygen combined water injection unit 88K is propelled to propulsion or the theoretical expansion engine 3P is driven to rotate the screw 7C. The aim is to make it easy to select water jet propulsion in the process of screw propulsion and exhaust, speed up the natural phenomenon in the process of propulsion and supply oxygen, nitrogen, CO2, etc. into the sea, microbial, phytoplankton, seagrass, coral and fish The present invention relates to a technology for various energy conservation cycle coalescence engines and coalescence methods, which increase human food, etc., and aim for the world's best profit rate.

洗脳皆無の小学校理科で考えると、既存最良蒸気タービン発電の大気圧同速度同容積仕事率kg重m/秒が、竪型全動翼比重大物質水銀重力タービン8N仕事率の1/2、3万と僅少に加えて、蒸気速度を堰止めて仕事皆無の静翼を動翼と交互に半分堰止め具備して、蒸気速度を1/100に近付けており加えて気体の体積が圧力に反比例するため、240気圧から大気圧まで240倍容積対応更に30、4mmHgまで25倍容積対応の、6000倍容積対応タービン翼が必要なため、理論的には高圧部蒸気速度が無茶苦茶低速で大革命が必要な背景があり、タービン翼面積対応に加えて、発電熱量全部で海水温度を7度上昇して海面全部を温度上昇自然現象不可能にし、上限の無い異常気象を増大し、50〜100年前後海水の豪雨等で人類が絶滅に近付く危険を増大中です。緑の地球は奇跡の産物で他の星に近付く危険が大きく、発電所側説明では海水温度上昇が7度以下なら環境に影響皆無としておりますが、例えば海水温度が30度の海域で7度上昇を継続すると、台風風速が300m/秒等になり海水の集中豪雨塩の被覆等で人類が絶滅する危険や、海面全部温度上昇して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、海中微生物や植物プランクトンや海草類を激減魚類等人類の海中食物も限り無く激減しており、中国が10%成長を続けると、海水温度上昇量は10年で現在の2倍20年で4倍と加速度的に増大して、最悪予想では台風や季節風や海上竜巻の風速が100m/秒等となり、海水を上空に吸引海水の集中豪雨として日本の農業や林業や居住地域が0に近付く等、50年前後で日本居住が困難になるため、手遅れ前に既存技術最悪部分に対応した技術開発が必要な背景がある。   Considering elementary school science without brainwashing, the existing best steam turbine power generation at atmospheric pressure and speed and volumetric capacity kg weight m / second is 1/2 of the gravity gravity turbine 8N power of the vertical type moving blade ratio critical material. In addition to a little, the steam speed is dammed and the stationary vanes with no work are half dammed with the moving blades, the steam speed is close to 1/100, and the gas volume is inversely proportional to the pressure. Therefore, it is necessary to have a turbine blade that can handle 240 times volume from 240 atmospheres to atmospheric pressure, and 30 times 4 mmHg, and 25 times capacity, and 6000 times capacity turbine blades. In addition to responding to the turbine blade area, the seawater temperature is raised by 7 degrees with all the heat generation, making the whole sea surface temperature-increasing natural phenomenon, increasing abnormal weather without an upper limit, 50-100 Around the year due to heavy rains of seawater Louis is in increasing the risk of closer to extinction. The green earth is a miracle product and there is a great risk of approaching other stars. According to the explanation of the power station, if the rise in seawater temperature is 7 degrees or less, there is no influence on the environment, but for example, 7 degrees in the sea area where the seawater temperature is 30 degrees If the rise continues, the typhoon wind speed will be 300m / sec, etc., and there will be danger of human beings extinction due to the covering of concentrated rainwater salt in seawater, etc., and the temperature of the whole sea surface will rise and nutrients such as nitrogen, oxygen, CO2 etc. The natural phenomenon that has supplied water is made impossible, the number of marine microorganisms, phytoplankton and seagrass is drastically reduced. The number of marine foods such as fish is drastically reduced. If China continues to grow 10%, the rise in seawater temperature will be 10%. The current rate is twice as high as the current rate in 20 years, and the speed of typhoons, seasonal winds and ocean tornadoes is 100m / sec. And forestry and residential areas Such as close to 0, for Japan residents it is difficult before and after 50 years, there is a background necessary technical development that corresponds to the existing technologies worst part before it's too late.

大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン発電の2.3万倍比重大物質水銀仕事率にして、真空中水銀重力加速度発電にすると、同速度1/100容積仕事率が既存蒸気タービン発電の230倍仕事率発電ですが、高さ500m以上に100台で23000倍発電量等膨大な発電量が予想され、燃料費0発電の無限大発電にし、竪型全動翼比重大物質水銀重力タービン8N発電円筒内側動翼群60C円筒外側動翼群60Dとして、夫々円筒組立固定動翼群を含めて全自動加工容易や組立容易や部品数1/10等にし、1/10部品全自動加工100台組立で23000倍発電量狙いにして、地球最大の真空中重力加速度加速の水銀重力エネルギで駆動し、大量の水銀資源による燃料費0発電で安価電気の用途拡大に移行して、太陽光加熱器21により空気を太陽光加熱し、水銀重力タービン8N燃料費0発電電気駆動の、1〜複数段二重反転圧縮機3T等熱ポンプ1Gで複数回圧縮複数回熱回収して、24〜200MPa過熱蒸気温熱50+液体空気冷熱28aに分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより供給して、液体酸素室5Kや蓄電池等に受給し、液体空気駆動の自動車や飛行機や船舶を1/10燃料費駆動や10倍速度駆動にして、極端に安価な発電の蓄電池駆動や電気駆動や、CO2排気僅少の地球温暖化防止が得られる背景がある。 When the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, are set to 23,000 times higher than that of the existing steam turbine power generation, and the mercury mercury acceleration in the vacuum, the mercury gravity acceleration power generation in the vacuum, the same speed 1/100 volume work The power generation rate is 230 times higher than that of the existing steam turbine power generation. However, enormous power generation such as 23000 times power generation is expected with 100 units at a height of 500m or more, and it will be an infinite power generation with zero fuel cost. Blade specific material mercury gravity turbine 8N power generation cylinder inner rotor blade group 60C cylinder outer rotor blade group 60D, each including cylindrical assembly fixed rotor blade group, fully automatic processing, easy assembly, 1/10 number of parts, etc. / 10 parts fully automatic processing 100 units assembled, aiming for power generation of 23,000 times, driven by mercury gravity energy with acceleration of gravitational acceleration in the world's largest vacuum, to expand the usage of low-cost electricity with zero fuel cost generation with a large amount of mercury resources Migrate The solar heater 21 heats the air into sunlight and compresses the heat multiple times with a heat pump 1G such as a 1-multistage counter-rotating compressor 3T with a mercury gravity turbine 8N fuel cost 0 power generation electric drive. , 24 to 200 MPa Superheated steam temperature 50 + liquid air cooling heat 28a divided and stored, supplied from electricity + liquid air cooling heat + superheated steam temperature supply equipment 3D, received in the liquid oxygen chamber 5K, storage battery, etc., liquid air driven automobile In addition, there is a background in which a 1/10 fuel cost drive or a 10 times speed drive of an airplane or a ship can be used to drive an extremely inexpensive power storage battery or electric drive, and to prevent global warming with little CO2 exhaust.

高校や大学では既存エンジンを理論最良エンジンと説明しており、洗脳皆無の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る。そこで例えば竪型全動翼比重大物質重力タービン8N発電にすると燃料費0安価発電になる背景があり、日本近海や永久凍土地下に眠る膨大なメタンハイドレートを加熱する場合を、小学校理科で考えると燃料費0加熱が最良です。そこで燃料費0発電電気駆動太陽光加熱器21にして、太陽光で加熱の空気28aを燃料費0発電電気駆動の、1〜複数段二重反転圧縮機3T等熱ポンプ1Gや1〜複数段圧縮熱回収器2Cで、複数回圧縮複数回熱回収し、冷熱の液体酸素5Kや液体窒素5L+温熱の過熱蒸気50に分割保存して、温熱利用無限大の過程で例えば、永久凍土地下のメタンハイドレートに過熱蒸気50を注入メタンと水に分割し、メタンを液体窒素冷却液体メタンで回収して過熱蒸気注入を永遠に継続して、メタン回収囲い内を適温で水滴の多い牧草地放牧とし、人類の食糧増大温熱利用無限大にして、液体空気駆動の自動車や船舶や宇宙往還機全盛として宇宙到達費用1/50万狙いにし、船舶駆動の過程では自然現象高速化2aして、微生物や海草類やサンゴ等を増殖食物連鎖等で魚類等人類の食物を増大し、海水の豪雨を阻止して人類絶滅を先送り出来る背景があり。燃料費僅少で10倍速度狙いの船舶革命や飛行機革命となって、運用利益率が既存運用利益率の10倍等膨大となり、世界規模100%独占した製造運用とし、雇用を増大する雇用増大革命に出来る背景がある。   In high school and university, the existing engine is described as the best engine, and when we return to elementary school science without brainwashing and think about the best engine, the unit of work is kg weight m / sec. The engine is the best engine in terms of generating rotational output at a high speed, but there is no trace of thought. Therefore, for example, if a vertical turbine blade-type critical material gravity turbine 8N power generation is used, there is a background that the fuel cost is low and power generation is low, and the case of heating enormous methane hydrate sleeping in the sea near Japan or permafrost is considered in elementary school science. And fuel cost 0 heating is the best. Therefore, the heat pump 1G such as a 1-multiple counter-rotating compressor 3T or 1-multiple stage of the fuel cost 0 power generation electric drive is made by using the solar heating air 28a as the fuel cost 0 power generation electric drive solar heater 21. Compressed heat recovery unit 2C compresses the heat multiple times, collects and stores in cold liquid oxygen 5K, liquid nitrogen 5L + hot superheated steam 50, and in the process of infinite use of heat, for example, methane under permafrost The superheated steam 50 is injected into the hydrate and divided into methane and water, and the methane is recovered with liquid nitrogen cooled liquid methane, and the superheated steam injection is continued forever to make the methane recovery enclosure grazing at a suitable temperature and with many water droplets. , Increase the use of heat by humans, make liquid air driven cars, ships and spacecrafts prime, aiming to reach 1 / 500,000 in space, speeding natural phenomena 2a in the process of driving ships, Seaweeds Gore, etc. to increase the food of fish such as the human race in the growth the food chain, etc., to prevent the heavy rain of sea water there is a background that can put off the human race extinct. Revolution of employment growth that will increase the employment by making the manufacturing operation monopolized 100% worldwide, with the operating profit rate becoming 10 times larger than the existing operational profit ratio, as the ship revolution and airplane revolution aiming at 10 times speed with low fuel cost There is a background that can be.

日本国特許1607151号、特許1609617号、特許1645350号、特許1924889号、特許1912522号、特許1959305号、特許1986119号、特許2604636号、1992年米国特許5133305号、1993年米国特許5230307号、1995年米国特許5429078号、1997年米国特許5701864号、PCT国際出願番号PCT/JP97/01814号・米国特許第6119650号、中国特許第8818号、EU英国特許902175号、PCT国際出願番号PCT/JP97/02250号・米国特許第6263664号がある。Japanese Patent No. 1607151, Patent No. 1609617, Patent No. 1645350, Patent No. 1924889, Patent No. 1912522, Patent No. 1959305, Patent No. 1986119, Patent No. 2646636, 1992 U.S. Pat. No. 5,133,305, 1993 U.S. Pat. US Pat. No. 5,429,078, 1997 US Pat. No. 5,701,864, PCT International Application No. PCT / JP97 / 01814, US Pat. No. 6,119,650, Chinese Patent No. 8818, EU British Patent No. 902175, PCT International Application No. PCT / JP97 / 02250 No. 6,263,664.

PCT国際出願公開NO.WO 2010/101017 PCT/JP2010/052171等は、特願2009−048869号出願日平成21年3月3日から特願2010−007805号出願日平成22年1月18日まで326個の出願があり、以後PCTを含めて特願2011−107954号出願日平成23年9月30日まで15個の出願があります。PCT International Application Publication No. WO 2010/101017 PCT / JP2010 / 052171 etc. have 326 applications from the date of filing of Japanese Patent Application No. 2009-048869 on March 3, 2009 to the date of filing of Japanese Patent Application No. 2010-007805 on January 18, 2010 Since then, there have been fifteen applications including PCT until September 30, 2011, the filing date of Japanese Patent Application No. 2011-107954.

既存世界の火力原子力発電所では、発電熱量全部で海水温度摂氏7度上昇海水温度上昇量を100年で1000倍等とし、下降気流や上昇気流を限り無く増大して、異常乾燥山火事や砂漠化や集中豪雨や熱波や寒波等を限り無く増大し、日本近海は20年前後で台風や季節風や竜巻を100m/秒等として、海水を上空に吸引海水の集中豪雨等により陸地に塩の被覆を設けて人類陸上食物減少の危険を増大し、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、微生物や植物プランクトンや海草類やサンゴ等を激減、食物連鎖等により魚類を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/秒等上限の無い異常気象の巨大化とし、海底岩盤膨張地震や津波を巨大化東日本の地震津波も巨大化して、人類絶滅の危険を増大のため海水の豪雨等を阻止し、海水温度上昇0等地球温暖化防止して、人類絶滅を先送りする課題がある。又最近の課題は財政赤字国の急増です。最大原因は安価労働コスト国を世界の工場として簡単に利益を得る流行蔓延で、簡単に利益が得られる半面途上国全部が過去の日本のように物真似改良で世界一を競うため、安価優良製品続出して先進国製造設備壊滅財政赤字増大雇用壊滅の危険があり、今の先進国経済危機は初期段階のため先進国利益率上昇発明が急務で、物真似改良が可能な発明実施は時代遅れと認識し、世界規模100%独占を永遠に続ける発明品の極秘製造極秘運用として、利益率抜群の世界一永遠にする課題がある。   In the existing thermal power plants in the world, the total heat generation is 7 degrees Celsius, and the seawater temperature rise is 1000 times in 100 years, and the downdrafts and updrafts are increased as much as possible. As the number of storms, torrential rains, heat waves, cold waves, etc. increases without limit, typhoons, seasonal winds, tornadoes, etc., around 100 years in the sea near Japan, salt water on the land due to concentrated heavy rains, etc. Covering increases the danger of human land food loss, making it impossible for the natural phenomenon of supplying nutrients to the sea-cooled seabed in winter, dramatically reducing microorganisms, phytoplankton, seaweeds, corals, etc., fish through food chains, etc. The number of human underwater foods has been reduced as much as 1/100, and droughts, torrential rains, typhoons and seasonal winds have increased 10 times in 100 years. For example, typhoons and seasonal winds have an upper limit such as 300m / sec. weather Giant seafloor bedrock expansion earthquakes and tsunamis, and eastern Japan earthquakes and tsunamis have also become huge, preventing heavy rain in seawater to increase the danger of human extinction, preventing global warming such as rising seawater temperature, There is a challenge to postpone human extinction. A recent issue is the rapid increase in countries with deficits. The biggest cause is the epidemic that easily makes profits with low labor cost countries as the world's factories, and all the developing countries that can easily make profits compete for the best in imitation improvement like Japan in the past, so cheap and excellent products There is a risk of the destruction of manufacturing facilities in the developed countries and the deficit of jobs in the developed countries, and the destruction of employment.There is an urgent need to increase profit margins in developed countries because the current economic crisis is in the early stages. However, as a top-secret manufacturing operation of an invention that continues to be a 100% monopoly on a global scale forever, there is a problem that makes the world eternal with an outstanding profit rate.

竪型全動翼比重大物質重力タービン8N燃料費0発電安価電気駆動全部にして、太陽光加熱器21+1〜複数段二重反転圧縮機3T等熱ポンプ1G+1〜複数段圧縮熱回収器2Cにより熱製造し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとして、受給した液体酸素5Kを圧縮して空気圧縮の21/60000容積圧縮仕事率とし、超高圧燃焼や超高温燃焼が容易な理論燃焼室4Yとして、例えば酸素アセチレンバーナー複数中心付近燃焼で外周付近高圧高温過熱蒸気50を加熱し、酸素アセチレン炎3000℃以上燃焼で過熱蒸気の熱分解狙い酸素水素増大燃焼狙いにして、4Y駆動の理論膨張機関3Pや酸素合体水噴射部88Kや酸素合体空気噴射部88Aとし、自動車等車両類や船舶類や飛行機類を回転力駆動や噴射推進駆動して、船舶類噴射推進駆動では自然現象高速化2aし、海中に酸素や窒素やCO2等を供給して、微生物や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、飛行機はCO2排気0に近い宇宙飛行全盛1日に地球を16周する等として、地球上何処でも日帰り旅行や大気中はCO2排気僅少飛行狙いとし、世界規模100%独占して極秘製造極秘運用する発電や船舶や飛行機として、利益率抜群の世界一や新規雇用抜群の世界一にし、旱魃や集中豪雨や台風や季節風や海水の豪雨や地震津波の巨大化を阻止して、地球温暖化防止し人類絶滅を先送りする。 Vertical type moving blade ratio critical material gravity turbine 8N fuel cost 0 power generation cheap electric drive all, heat by solar heater 21 + 1 ~ multistage counter rotating compressor 3T etc. heat pump 1G + 1 ~ multiple stage compression heat recovery unit 2C Manufactured as electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D, the received liquid oxygen 5K is compressed to 21/60000 volumetric compression work rate of air compression, and theoretical combustion that is easy for ultra high pressure combustion and ultra high temperature combustion As the chamber 4Y, for example, the high temperature high temperature superheated steam 50 is heated near the outer periphery in the combustion near the center of the oxygen acetylene burner, the thermal decomposition of the superheated steam is aimed at the combustion of the oxygen acetylene flame at 3000 ° C. or more, and the oxygen hydrogen increase combustion is aimed at. The expansion engine 3P, the oxygen combined water injection unit 88K, and the oxygen combined air injection unit 88A are used to drive vehicles such as automobiles, ships, and airplanes, and to drive the rotational force and drive the injection. The ship jet propulsion drive speeds up natural phenomena 2a, supplies oxygen, nitrogen, CO2, etc. into the sea, increases microorganisms, phytoplankton, seaweeds, corals, fish, etc., and increases human food. Power generation and ships that operate 100% of the world's scale and have top secret manufacturing operations, aiming for a day trip anywhere on the earth and aiming for a small amount of CO2 exhaust in the atmosphere, such as making 16 orbits of the earth on a full day of space flight close to zero exhaust. As an aircraft and airplane, it is the best in the world for profit margins and the best for new jobs, preventing droughts, torrential rains, typhoons, seasonal winds, heavy rains on seawater, and earthquakes and tsunamis to prevent global warming and extermination of humanity Postpone.

比重大物質重力タービン8N燃料費0安価発電の、横軸1h二重反転を100台等に伝達する効果が非常に大きく、円筒動翼群60C60D2種類の理論最良タービン翼8cを、100台分全自動製造で100台製造の効果も非常に大きく、ボイラや原子炉が不要で構造が簡単になる効果も非常に大きく、既存蒸気タービン最終動翼群の羅列に近い竪型全動翼水重力タービン8M発電を、最大速度の最終動翼群と同真空駆動で比較説明すると、大気圧100℃760mmHgで水の1700倍容積の水蒸気は、排気温度29℃真空度30mmHgでボイルの法則により、760mmHg×1700=30mmHg×V2倍容積の水蒸気となり、V2=760/30×1700=水の43000倍容積水蒸気となります。即ち既存蒸気タービン最高速度仕事率動翼群を羅列する、竪型全動翼水重力タービン8M発電が出力発生段階で遥かに優位に加えて、過熱蒸気の1/100容積水速度で430倍発電量になるのに加えて、真空度上昇も遥かに優位で、真空中の重力加速度利用は更に100台重ねた1台で43000倍発電量を算出に加えて、ウォータージェット加工機水噴射速度マッハ3で水噴射すると更に3倍発電量が算出される等、実験が必要ですが発電原価を1/10等に大改革する大革命に非常に大きな効果がある。 Specific gravity material gravity turbine 8N Fuel cost 0 Low cost power generation, the effect of transmitting the horizontal axis 1h double reversal to 100 units, etc. is very large, all the 100 best turbine blades 8c of the cylindrical blade group 60C60D The 100-unit automatic manufacturing process is very effective, the boiler and nuclear reactor are not required, and the effect of simplifying the structure is very large. Comparing the 8M power generation with the maximum speed final blade group in the same vacuum drive, the water vapor of 1,700 times the volume of water at an atmospheric pressure of 100 ° C. and 760 mmHg is 760 mmHg × according to Boyle's law at an exhaust temperature of 29 ° C. and a vacuum degree of 30 mmHg. 1700 = 30mmHg x V2 volume water vapor, V2 = 760/30 x 1700 = water 43,000 times water vapor. In other words, the vertical-type full-blade water gravity turbine 8M power generation lined up with the existing steam turbine maximum speed power blade group is far superior in the output generation stage, and 430 times power generation at 1/100 volume water speed of superheated steam In addition to increasing the amount of vacuum, the increase in the degree of vacuum is far superior, and the use of gravitational acceleration in a vacuum is further increased by 43,000 times the power generation rate in one unit with 100 additional units, and the water jet speed Mach Experiments are necessary, such as calculating the amount of power generation three times when water is injected at 3, but it has a great effect on the major revolution that greatly reforms the power generation cost to 1/10.

緑の地球は奇跡の産物で他の星に近付く危険が大きく、例えば中国が10%成長を100年続けると、火力発電や原子力発電により中国近海の海水温度上昇量が1000倍を超えるため、現在日本のゲリラ豪雨増大が海水の豪雨1000倍等となり、現在の魚類激減が0に近付く等人類絶滅が100年以内に急接近する可能性が強く、海水温度上昇0やCO2排気0や燃料費0発電電気駆動が必要です。そこで燃料費0発電電気製造の電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより液体酸素室5Kに受給して、燃焼用酸素の圧縮仕事率を空気圧縮の21/60000容積圧縮仕事率にし、理論燃焼室4Y中心付近高温燃焼で過熱蒸気50の熱分解や理論燃焼室4Yの保護として、理論燃焼室4Yにより理論膨張機関3Pや酸素合体水噴射部88Kや酸素合体空気噴射部88Aを、最も効率良く駆動出来る効果があり、自動車や船舶や飛行機を燃料費1/10や10倍速度等が狙える効果に加えて、宇宙到達経費を既存宇宙ロケットの1/50万経費狙いに出来る効果があり、車輪やスクリュー7Cやプロペラ7Aや回転翼7Bを理論膨張機関3P駆動し、船舶や飛行機や自動車等を回転力駆動して、船舶噴射推進駆動では自然現象高速化2aし、水中微生物のCO2等の消化能力を森林の数万倍狙い等に増大する効果が大きく、植物プランクトンや海草類やサンゴ等を増殖して、食物連鎖等で魚類等人類の海中食物を大増大し、砂漠化や旱魃や集中豪雨や台風や季節風や地震津波等の巨大化を阻止して、人類で最も重要な人類絶滅を先送りし、利益率抜群世界一を狙える効果がある。 The green earth is a miracle product and has a high risk of approaching other stars. For example, if China continues to grow 10% for 100 years, the temperature rise in the sea near China will exceed 1000 times due to thermal power generation and nuclear power generation. There is a strong possibility that the extinction of mankind will rapidly approach within 100 years, such as the increase in guerrilla heavy rain in Japan is 1000 times the heavy rain in seawater, the current drastic decrease in fish is close to 0, and seawater temperature rises 0, CO2 emissions 0 and fuel costs 0 Electric power drive is required. Therefore, the fuel cost is 0. Electricity generated by power generation electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D is received into the liquid oxygen chamber 5K, and the compression work rate of combustion oxygen is set to 21/60000 volumetric compression work rate of air compression, As the thermal decomposition of the superheated steam 50 and the protection of the theoretical combustion chamber 4Y in the high temperature combustion near the center of the theoretical combustion chamber 4Y, the theoretical expansion chamber 3Y, the oxygen combined water injection unit 88K and the oxygen combined air injection unit 88A are most It has the effect of being able to drive efficiently, and in addition to the effect that automobiles, ships and airplanes can be aimed at fuel costs of 1/10 or 10 times the speed, the effect of being able to target the space arrival cost to 1 / 500,000 of existing space rockets The wheels, screws 7C, propellers 7A and rotor blades 7B are driven by the theoretical expansion engine 3P to drive the rotational force of ships, airplanes, automobiles, etc. a. The effect of increasing the digestive capacity of underwater microorganisms such as CO2 to tens of thousands of times of the forest is great, and phytoplankton, seaweeds, corals, etc. are proliferated, and fish and other marine foods such as fish are greatly increased in the food chain. It will increase, preventing desertification, droughts, torrential rains, typhoons, seasonal winds, earthquake tsunamis, and so on, postponing the most important human extinction of humanity and aiming for the world's best profit rate.

飛行機駆動は、燃料費0竪型全動翼比重大物質重力タービン8N発電電気駆動の、電気+液体空気冷熱+過熱蒸気温熱供給設備より液体酸素を受給し、液体酸素5K+液体燃料1c+水52aを超高圧圧縮して、液体燃料制御弁1K+液体酸素制御弁5T+水制御弁5Qを開放最適温度に加熱し、酸素ガス+燃料ガス複数個所中心付近混合噴射着火燃焼外周高圧高温過熱蒸気を過熱して、最高温度燃焼理論燃焼室4Y保護燃焼過熱蒸気熱分解燃焼狙い酸素水素増大燃焼狙いにし、酸素合体空気噴射部88Aを駆動して、宇宙到達費用を既存宇宙ロケットの1/50万経費狙いにし、同一燃料費10倍噴射推進出力で宇宙利用全盛を狙う効果があり、例えば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、大気中は燃料費僅少のプロペラ飛行や回転翼飛行や噴射推進狙いにし、水蒸気噴射速度や燃焼ガス噴射速度が真空中で最大のため、既存宇宙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、50〜200MPaの高圧高温燃焼ガス5M+高圧高温水蒸気5Nの噴射量増大にして、1日に地球を16周する等とし、地球上何処でも日帰り旅行が可能な宇宙利用全盛を狙える効果がある。 Airplane drive receives liquid oxygen from the electricity + liquid air cold heat + superheated steam temperature heat supply facility of the fuel drive 0 type all blades important material gravity turbine 8N power generation electric drive, liquid oxygen 5K + liquid fuel 1c + water 52a Super high pressure compression, the liquid fuel control valve 1K + liquid oxygen control valve 5T + water control valve 5Q is heated to an optimal temperature, and oxygen gas + fuel gas near the center of the mixed injection ignition combustion outer periphery high pressure high temperature superheated steam is heated. , The highest temperature combustion theory combustion chamber 4Y protection combustion superheated steam pyrolysis combustion aiming oxygen oxygen increased combustion aiming, driving the oxygen coalesced air injection unit 88A, aiming for space arrival cost 1 / 500,000 of existing space rocket, It has the effect of aiming at the prime of space utilization with the same fuel cost 10 times propulsion propulsion output. For example, the injection propulsion output is 100 times the pressure of existing jets 10 times the calorific value injection 1000 times the short time As an output target, in the atmosphere, propeller flight, rotor blade flight and injection propulsion aiming at low fuel costs, the steam injection speed and combustion gas injection speed are the largest in vacuum, so the existing space rocket ground mass injection is considered the worst, Space use that allows one-day trip anywhere on the earth by increasing the injection amount of high-pressure high-temperature combustion gas 5M + high-pressure high-temperature steam 5N of 50-200MPa from the vicinity of the highest flight altitude of existing aircraft, and making 16 rounds of the earth a day. There is an effect that can be aimed at the prime.

竪型全動翼比重大物質重力タービン8Nの1h9C9Bの説明図(実施例1)Explanatory drawing of 1h9C9B of vertical type moving blade ratio critical material gravity turbine 8N (Example 1) 円筒動翼群60の60E60F60G60H60J60Kの説明図(実施例2)Explanatory drawing of 60E60F60G60H60J60K of the cylindrical blade group 60 (Example 2) 電気+液体冷熱+温熱供給設備3Dの太陽光加熱器21の説明図(実施例3)Explanatory drawing of the solar heater 21 of electricity + liquid cold / heat supply equipment 3D (Example 3) 理論気体圧縮機3Tの9B9C9D9E6F6G6Hの説明図(実施例4)Explanatory drawing of 9B9C9D9E6F6G6H of theoretical gas compressor 3T (Example 4) 理論膨張機関3Pの5b6X6Y9B9C9D9E5の説明図(実施例5)Explanatory drawing of 5b6X6Y9B9C9D9E5 of the theoretical expansion engine 3P (Example 5) 酸素合体水噴射部88Kの説明図(実施例6)Explanatory drawing of oxygen combined water injection part 88K (Example 6) 酸素合体空気噴射部88Aの説明図(実施例7)Explanatory drawing of oxygen combined air injection part 88A (Example 7) 理論膨張機関自動車4Kの説明図(実施例8)Explanatory drawing of theoretical expansion engine automobile 4K (Example 8) 酸素合体スクリュー船舶39Hの説明図(実施例9)Explanatory drawing of oxygen coalescence screw ship 39H (Example 9) 酸素合体スクリュー噴射船舶39Kの説明図(実施例10)Explanatory drawing of the oxygen coalescence screw injection ship 39K (Example 10) 酸素合体噴射船舶39Jの説明図(実施例11)Explanatory drawing of the oxygen coalescence injection ship 39J (Example 11) 酸素合体噴射飛行機39Lの説明図(実施例12)Explanatory drawing of oxygen coalescence injection plane 39L (Example 12) 酸素合体プロペラ飛行機39Mの説明図(実施例13)Explanatory drawing of oxygen combination propeller plane 39M (Example 13)

既存蒸気タービン発電等洗脳で長期間真空中の重力加速度利用が阻止され、100台重ねた1台で既存蒸気タービン発電1台の43000倍発電量狙い等を阻止して、例えば既存最良蒸気タービン発電の大気圧同速度同容積仕事率kg重m/秒を、水仕事率の1/1700と僅少にし、静翼を動翼と交互に設けて堰き止めて回転出力を0に近付け、蒸気タービン発電の駆動熱量全部で海水温度7度上昇魚類激減、海底岩盤を膨張地震や津波を巨大化し、20年前後で日本近海の台風や季節風や海上竜巻の上昇気流を巨大化100m/秒等にして、海水を上空に吸引海水の豪雨が予想される等、50〜100年前後で陸地に塩の被覆を設けて食糧激減人類絶滅が急接近する危険があります。即ち既存技術の致命的欠点多数で発明が膨大になり過ぎるため、発明を符号の説明に記載すると共に、先の出願で再三説明した部分は省略し、横軸1h二重反転竪型全動翼比重大物質重力タービン8N以外を3種類実施例で代用説明して、常識を省略した発明の具体化に挑戦します。     The use of gravity acceleration in a vacuum for a long period of time is prevented by brainwashing such as existing steam turbine power generation, and one unit of 100 units prevents the aim of generating power 43,000 times that of one existing steam turbine power generation, for example, the existing best steam turbine power generation Steam pressure is reduced by reducing the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, to 1/1700 of the water power, and by installing the stationary blades alternately with the moving blades and blocking the rotation output to zero. The seawater temperature rises by 7 degrees with all of the driving heat of the sea, the fishes drastically decrease, the bottom bedrock expands into earthquakes and tsunamis, and the typhoons, seasonal winds and sea tornadoes around Japan are increased to around 100 m / sec. There is a danger that food extinctions and humankind extinction will be approaching rapidly by providing salt coating on the land in around 50 to 100 years, such as heavy rain of suction seawater is expected over the sea. That is, since the invention becomes too large due to many fatal defects of the existing technology, the description of the invention is described in the description of the reference, and the part which has been repeatedly described in the previous application is omitted, and the horizontal axis 1h counter-rotating vertical type whole moving blade We will try to materialize the invention by omitting common sense by explaining with 3 kinds of examples other than specific gravity gravity turbine 8N.

図1竪型全動翼比重大物質重力タービン8N発電量がkg重m/秒に比例するため、内側軸装置60A外側軸装置60Bに夫々反発永久磁石9B吸引永久磁石9Cを具備し、夫々の重量を反発力や吸引力により0に近付け軸受荷重を0接近にして、リング型両面2極着磁複数具備で回転速度や回転外径の無限増大狙いにし、比重大物質上昇装置2Fにより比重大物質2E3Eを500〜828m等上昇して、比重大物質加速機6Wで比重大物質3Eをマッハ3以上噴射狙い2Eを混合噴射にし、比重大物質の重力加速度加速真空加速の円筒内側動翼群60C円筒外側動翼群60D回転にして、横軸1h歯車で二重反転次々に100組等駆動する竪型全動翼比重大物質重力タービン8N発電にし、内側軸装置60A外側軸装置60Bに円筒部を夫々具備して、全自動加工容易や組立容易にし、重力加速度加速真空加速駆動する動翼群を円筒環状組立9Aに嵌合構成して、円筒内側動翼群60Cや円筒外側動翼群60Dとして横軸1h二重反転駆動し、空気抽出器51を気体専用冷却室11Dに具備水の摩擦熱を冷却最高真空にして、製造過程では円筒内側動翼群60Cや円筒外側動翼群60D夫々を図2のように、入口固定外翼60E+入口固定内翼60F+外側環状翼60G+内側環状翼60H+出口固定外翼60J+出口固定内翼60Kとし、6部品を夫々全自動鋳造や全自動加工や超硬合金表面処理等で100組製造等として、円筒環状組立9A等安価大量生産容易とボイラや原子炉不要にし、重量を支持する永久磁石や電磁石を含む推力軸受80aや軸受80として、水を真空加速する重力加速部1gを具備し、重力加速部1g継ぎ手には発電機1を駆動する横軸1h貫通穴を具備して、発電機1をタービン外箱77aの外で複数駆動とし、多段竪型全動翼比重大物質重力タービン8N回転方向交互駆動して、重力加速部1g加速により次のタービン8Nを駆動次々に横軸1h交互駆動し、構造簡単安価な電気製造物無限多や電気駆動無限多にして、利益率抜群世界一の各種エネルギ保存サイクル合体機関発電及び合体方法発電にする。 FIG. 1 Since the power generation amount of the vertical-type full blade ratio critical material gravity turbine 8N is proportional to kg weight m / second, the inner shaft device 60A and the outer shaft device 60B are respectively provided with repulsive permanent magnets 9B attracting permanent magnets 9C, The weight is made close to 0 by the repulsive force and attractive force, the bearing load is made close to 0, the ring type double-sided double pole magnets are used to aim at infinite increase in rotational speed and rotational outer diameter, The material 2E3E is raised by 500 to 828 m, etc., and the specific critical material accelerator 6W aims to inject the specific critical material 3E to Mach 3 or more, and the 2E is mixed and injected. A cylindrical outer rotor blade group 60D is rotated, and a vertical type moving blade specific material gravity turbine 8N power generation is driven by 100 sets of double reversals one after another with a horizontal axis 1h gear, and a cylindrical portion is formed on the inner shaft device 60A and the outer shaft device 60B. The In order to facilitate fully automatic processing and assembly, a blade group that is driven by gravity acceleration acceleration and vacuum acceleration is fitted to the cylindrical annular assembly 9A to form a cylindrical inner blade group 60C and a cylindrical outer blade group 60D. The horizontal axis is 1h counter-rotating, the air extractor 51 is provided in the gas-only cooling chamber 11D, and the frictional heat of the water is cooled to the highest vacuum, and in the manufacturing process, the cylinder inner blade group 60C and the cylinder outer blade group 60D are respectively used. As shown in FIG. 2, the inlet fixed outer blade 60E + the inlet fixed inner blade 60F + the outer annular blade 60G + the inner annular blade 60H + the outlet fixed outer blade 60J + the outlet fixed inner blade 60K. 100 sets are manufactured by alloy surface treatment, etc., such as cylindrical annular assembly 9A, etc., easy to manufacture at low cost, no boilers or nuclear reactors are required, and as thrust bearings 80a and bearings 80 including permanent magnets and electromagnets that support weight, The gravity acceleration part 1g which accelerates | stimulates, the gravity acceleration part 1g joint is equipped with the horizontal-axis 1h through-hole which drives the generator 1, and the generator 1 is made into multiple drive out of the turbine outer casing 77a, and multistage Type full blade ratio material gravity turbine 8N rotation direction alternate drive, next turbine 8N driven by gravity acceleration part 1g acceleration one after another horizontal axis 1h alternate drive, simple structure and cheap electric product infinite and electric drive Infinitely, the world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profit rate.

竪型全動翼比重大物質重力タービン8N発電は、6部品を2種類の円筒環状組立9Aで1組として、タービン外箱77a内に既存最高建築物828mに100〜200組等垂直具備で1台とし、最下部内側軸装置60Aや外側軸装置60Bの大重量を支える推力軸受80aは特別仕様として、軸受80は普通仕様として夫々横軸1h歯車で二重反転歯車装置85Yを構成し、円筒内側動翼群60C円筒外側動翼群60Dをタービン毎交互回転の二重反転駆動して、共振を相殺したタービン駆動で振動や騒音を僅少とし、比重大物質加速器6Wによるウォータージェット加工機水速度のマッハ3〜1噴射速度、例えば水銀3E圧力で白金球2E混合噴射として、マッハ3等噴射で真空中重力加速度加速効果最高として円筒内側動翼群60C円筒外側動翼群60Dに噴射し、夫々を横軸1h二重反転駆動発電してマッハ3〜1速度を維持加速して、次のタービンを駆動して落差を有効利用する竪型全動翼比重大物質重力タービン8N発電にし、摩擦熱冷却して空気抽出器51で30mmHg等既存発電最高真空度以上容易として、落差828mに100〜200組使用とし、既存蒸気タービン発電の最終段真空度30mmHg水の43000倍容積マッハ1速度水蒸気として、100組重ねた1台のタービン8N発電量と比較説明すると、1/1000容積の水銀をマッハ1速度噴射で43×100×13、55=58265倍水銀発電量となり、白金球では91891倍白金球発電量の計算になる等実験が必要な天文学的倍率の発電量になる、各種エネルギ保存サイクル合体機関燃料費0極端に安価発電にする。 The vertical type moving blade ratio critical material gravity turbine 8N power generation consists of 6 parts in one set with two types of cylindrical annular assemblies 9A, and 100 to 200 sets such as 100 to 200 sets in the existing highest building 828m in the turbine outer box 77a. The thrust bearing 80a that supports the heavy weight of the lowermost inner shaft device 60A and the outer shaft device 60B is a special specification, and the bearing 80 is a normal specification. Inner rotor blade group 60C Cylindrical outer rotor blade group 60D is driven by double reversal for each turbine, and vibration and noise are reduced by turbine drive that cancels resonance. Water jet machine water speed by specific material accelerator 6W Mach 3 to 1 injection speed, for example, as a mixed injection of platinum spheres 2E with mercury 3E pressure, as a maximum effect of acceleration of gravity acceleration in vacuum with Mach 3 injection, etc. Sputtered side rotor blade group 60D, each horizontal axis 1h counter-rotating drive power generation, maintaining and accelerating Mach 3 to 1 speed, driving the next turbine to make effective use of the head Large-scale gravity turbine 8N power generation, friction heat cooling and air extractor 51 make it easy to exceed the existing power generation maximum vacuum level such as 30mmHg, use 100-200 sets in the drop 828m, final steam vacuum power generation 30mmHg water Compared with 100 turbines of one set of turbine 8N power generation capacity of 43,000 times volume Mach 1 speed steam, 1/1000 volume of mercury is 43 × 100 × 13, 55 = 58265 times mercury power generation by Mach 1 speed injection The energy saving cycle combined engine fuel cost, which will be the amount of power generation of astronomical magnification that requires experiments such as calculation of platinum ball power generation amount of 91891 times in platinum ball To be extremely inexpensive power generation.

図2の図1円筒内側動翼群60C円筒外側動翼群60Dの、円筒環状組立9Aで最も重要な構成は摩擦損失を最低が最重要なため、使用比重大物質に合せた摩擦損失低減被覆や耐摩耗被覆選択可能とし、内側軸装置60A+外側軸装置60B夫々に円筒環状組立9Aを具備して、外側軸装置60Bと円筒環状組立9Aを入口固定外翼60E環状嵌合組立固定で、円筒外側動翼群60Dの入口動翼群を構成し、内側軸装置60Aと円筒環状組立9Aを入口固定内翼60F環状嵌合組立固定で、円筒内側動翼群60Cの入口動翼群を構成して、外側軸装置60Bと円筒環状組立9Aを外側環状翼60G環状嵌合組立で、円筒外側動翼群60Dの中間動翼群を構成し、内側軸装置60Aと円筒環状組立9Aを内側環状翼60H環状嵌合組立で、円筒内側動翼群60Cの中間動翼群を構成して、外側軸装置60Bと円筒環状組立9Aを外側環状翼60G環状嵌合組立で、円筒外側動翼群60Dの中間動翼群2回目を構成し、内側軸装置60Aと円筒環状組立9Aを出口固定内翼60K環状嵌合組立固定で、円筒内側動翼群60Cの出口動翼群を構成して、外側軸装置60Bと円筒環状組立9Aを出口固定外翼60J環状嵌合組立固定で、円筒外側動翼群60Dの出口動翼群を構成し、6種類の円筒動翼群60を夫々100組以上全自動加工等で製造1台製造等として、構造簡単やボイラや原子炉不要等で製造原価を極端に安価とし、運用利益率も燃料消費0等比較物皆無の抜群世界一にする、竪型全動翼比重大物質重力タービン8N極端に安価発電にする。   2 of FIG. 2 The most important configuration of the cylindrical inner blade group 60C of the cylindrical inner blade group 60D in the cylindrical annular assembly 9A is that the lowest friction loss is the most important. The inner shaft device 60A and the outer shaft device 60B each have a cylindrical annular assembly 9A, and the outer shaft device 60B and the cylindrical annular assembly 9A are fixed to the inlet fixed outer wing 60E in an annular fitting assembly. The inlet rotor blade group of the outer rotor blade group 60D is configured, and the inner shaft device 60A and the cylindrical annular assembly 9A are configured by fixing the inlet fixed inner blade 60F annular fitting assembly, thereby forming the inlet rotor blade group of the cylindrical inner rotor blade group 60C. Thus, the outer shaft device 60B and the cylindrical annular assembly 9A are formed by the outer annular blade 60G annular fitting assembly to form an intermediate blade group of the cylindrical outer blade group 60D, and the inner shaft device 60A and the cylindrical annular assembly 9A are formed by the inner annular blade. 60H ring fitting assembly, cylinder The intermediate rotor blade group of the side rotor blade group 60C is constituted, and the outer shaft device 60B and the cylindrical annular assembly 9A are constituted by the outer annular blade 60G annular fitting assembly to constitute the second intermediate rotor blade group of the cylindrical outer rotor blade group 60D. Then, the inner shaft device 60A and the cylindrical annular assembly 9A are configured to fix the outlet fixed inner blade 60K in an annular fitting assembly, thereby forming an outlet blade group of the cylindrical inner blade group 60C, and the outer shaft device 60B and the cylindrical annular assembly 9A. Outlet fixed outer blade 60J Annular fitting assembly fixed to form the outer rotor blade group of the outer cylindrical blade group 60D, and 100 types of each of the six types of cylindrical blade groups 60 are manufactured by fully automatic processing, etc. As a result, the production cost is extremely low because of its simple structure, no boilers and no nuclear reactors, etc., and the operating profit rate is the world's best with no fuel consumption. To cheap power generation.

図3の太陽光加熱器21の熱製造は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気駆動で、安価な電気+液体空気冷熱+過熱蒸気温熱供給設備3Dにするもので、太陽光加熱器21を水面に浮力を設け又は平地に円形鉄道を設けて具備し、太陽光を東から西に直角維持回転制御する水上装置や陸上装置として、太陽光加熱器21には回転支持部4fを設けて歯車装置4dやローラー4eを具備し、円筒回転部77Gとして太陽光を上下方向直角維持回転制御して、浮力や円形鉄道利用により東西方向直角維持回転制御する装置とし、太陽光を2方向直角維持回転制御して、熱吸収管4H内空気温度を最高にする装置とし、地球最大熱量の太陽光を矩形長レンズ2dにより直線状に集めて、焦点距離付近に熱吸収管4H具備内部空気路28A空気28a温度を最高にして、外部空気路28A空気28a温度も上昇し、既存のレンズ断面を直線状に延長矩形の長レンズ2dとして、レンズ材質全部を使用可能とし、発泡プラスチック等の断熱材2cを円筒回転部77G等で囲って円筒等の長大な筒として、長大な長レンズ2dを継手80A+締付具80Bで密封上部を4H外部空気路28Aとし、2空気路28A選択吸入の1〜複数段熱ポンプ1Gとして吸入圧縮して、理論気体圧縮機3Tを熱ポンプ1Gとして800〜1200℃複数回とし、1〜複数段圧縮熱回収器2Cで圧縮毎熱回収を繰返して、液体空気28a冷熱を液体酸素室5K+液体窒素室5Lに保存し、400℃前後50〜200MPa過熱蒸気50温熱を高圧高温水蒸気室5Nに分割保存して、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dにし各種用途に使用して、電気駆動全盛や蓄電池駆動全盛にし、電気製造物の各種温熱利用全盛や各種冷熱利用全盛にする。 Heat production of the solar heater 21 in FIG. 3 is a vertical all-blade ratio critical material gravity turbine 8N fuel cost 0 power generation power generation extremely cheap electric drive, cheap electricity + liquid air cold heat + superheated steam temperature supply equipment 3D The solar heater 21 has a buoyancy on the surface of the water or a circular railroad on a flat surface, and the solar heater 21 is used as a surface device or a land device for rotating and controlling sunlight at right angles from east to west. Is provided with a rotation support part 4f and provided with a gear unit 4d and a roller 4e, and as a cylindrical rotation part 77G, the vertical rotation maintaining rotation is controlled at right angles in the vertical direction, and the east-west vertical rotation control is performed by using buoyancy and circular railway. The solar light is controlled to maintain the right angle in two directions and the air temperature in the heat absorption tube 4H is maximized, and the solar light with the maximum amount of the earth is collected in a straight line by the rectangular long lens 2d, and is near the focal length. Heat absorption tube 4H The internal air passage 28A air 28a temperature is maximized, the external air passage 28A air 28a temperature is also increased, and the existing lens cross section is linearly extended as a rectangular long lens 2d. A heat insulating material 2c such as a cylinder is surrounded by a cylindrical rotating portion 77G or the like to make a long cylinder such as a cylinder, a long long lens 2d is a joint 80A + fastener 80B, and a sealed upper part is a 4H external air passage 28A. Inhalation compression is performed as a 1 to multiple-stage heat pump 1G for suction, and the theoretical gas compressor 3T is set to 800 to 1200 ° C. multiple times as a heat pump 1G, and heat recovery for each compression is repeated in the 1-multistage compression heat recovery unit 2C. , Liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L, and 50-200 MPa superheated steam 50 warm heat around 400 ° C. is divided and stored in the high pressure high temperature steam chamber 5N. Electrical + liquid air cold + using various applications in the superheated steam heat supply facilities 3D, the electric drive flourish and battery driven prime, to various thermal utilization prime and various cold use PRIME electrical product.

図4の理論気体圧縮機3Tは超大型や超高速回転や圧縮比大幅増大狙う、反発永久磁石9B吸引永久磁石9C圧縮空気部9D真空部9E水噴射部6F具備して、磁力+空気圧利用で軸受荷重0接近や気化熱利用で1台の圧縮比大幅増大とし、ボイルの法則気体の体積は圧力に反比例する理論で最良狙いにして、円周長大圧縮翼から中心短圧縮翼に吸入圧縮することで吸入空気量最大狙いにし、全動翼二重反転圧縮翼の上側圧縮翼群8gや下側圧縮翼群8hで吸入空気速度最大狙いにして、組立圧縮翼群8jにより組立容易や吸入口面積最大容易や圧縮効率最良狙いにし、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気駆動として、横軸1h歯車の二重反転磁気(歯車)装置85(85Y)により、上側圧縮翼群8g下側圧縮翼群8hを夫々反対方向に回転する二重反転駆動にし、相対周速度を既存軸流圧縮機の3〜10倍狙い理論最良の理論気体圧縮機3Tとして、最終圧縮翼6静翼6Gより圧縮空気熱交換器2Yに圧入する熱製造とし、主として太陽光加熱器2の加熱空気を、理論気体圧縮機3Tの熱ポンプ1Gで圧縮高温として、圧縮高温毎に1〜複数段圧縮熱回収器2Cで熱回収し、液体空気冷熱+過熱蒸気温熱として分割保存して、電気+液体空気冷熱+過熱蒸気温熱の供給設備3Dとし、安価な過熱蒸気は炊飯やメタンの回収や温室栽培等無限加熱用途に使用として、安価な液体酸素は圧縮仕事率を空気圧縮の21/60000にした自動車や船舶や飛行機駆動とし、安価な液体窒素は氷製造等冷却用途無限使用等として、各種用途に使用します。 The theoretical gas compressor 3T of FIG. 4 is equipped with a repulsive permanent magnet 9B attracting permanent magnet 9C compressed air part 9D vacuum part 9E water injection part 6F aiming at super large size, super high speed rotation and a large compression ratio, and using magnetic force + air pressure The compression ratio of one unit is greatly increased by approaching zero bearing load or using heat of vaporization, and Boyle's law gas volume is suction-compressed from the large circumferential compression blade to the central short compression blade with the best aim in theory that is inversely proportional to pressure. The maximum intake air amount is aimed at, and the intake air speed is aimed at the maximum in the upper compression blade group 8g and the lower compression blade group 8h of all the rotor blades counter-rotating compression blades. Easy to reach the maximum area and compression efficiency, aiming at the best material ratio of vertical blades, gravity turbine 8N, fuel cost, 0 power generation, extremely low-priced electric drive, 1h horizontal axis reverse gear (gear) device 85 (85Y) , Upper compression blade group 8g lower side From the final compression blade 6 stationary blade 6G as the best theoretical gas compressor 3T, aiming at a relative peripheral speed of 3 to 10 times that of the existing axial flow compressor, and rotating the contracted blade group 8h in opposite directions, respectively. The heat production is press-fitted into the compressed air heat exchanger 2Y, and the heated air of the solar heater 2 is mainly compressed at a high temperature by the heat pump 1G of the theoretical gas compressor 3T. Heat recovered at 2C, divided and stored as liquid air cold heat + superheated steam temperature, and used as 3D electricity + liquid air cold heat + superheated steam temperature supply equipment. Inexpensive heating such as rice cooking, methane recovery and greenhouse cultivation for inexpensive superheated steam Inexpensive liquid oxygen is used for various purposes such as driving automobiles, ships and airplanes with a compression work rate of 21/60000 of air compression, and cheap liquid nitrogen is used for infinite cooling applications such as ice production. The

図5の水素+酸素増大燃焼狙う理論膨張機関3Pは、超大型や超高速回転等超安価回転出力狙う、反発永久磁石9B吸引永久磁石9C圧縮空気部9D真空部9E具備して、磁力+空気圧利用で軸受荷重0接近とし、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+過熱蒸気を受給して、液体酸素5Kを圧縮することで、圧縮容積仕事率を空気圧縮の21/60000容積圧縮仕事率にし、液体酸素5K+液体燃料1c+水52aを24〜200MPa等超高圧に圧縮して、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放理論燃焼室4Y内壁で最適温度に加熱し、過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放、例えば酸素アセチレンバーナー複数中心付近3000℃以上燃焼で外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、内壁で最適温度に加熱した過熱蒸気50や燃料や酸素として、内壁の保護燃焼や超高圧高温燃焼にし、燃焼ガス噴射ノズル6Yより燃焼ガス49等噴射して、圧縮吸入空気路5b空気噴射ノズル5の圧縮空気又は吸入空気を吸引噴射し、燃料管25c燃料噴射ノズル6Xより燃料噴射燃焼燃焼量大幅に増大して、燃料燃焼量を増大する理論膨張機関3P駆動にし、燃焼ガス49を高圧高温燃焼ガス49として中心から円周方向380度噴射して、上側膨張翼群8d下側膨張翼群8e最適箇所噴射横軸1h二重反転駆動とし、ボイルの法則気体の体積は圧力に反比例する理論で最良の理論膨張機関3Pとして、タービン外箱77a組立タービン翼群8fより噴射する理論膨張機関3Pとする。 The theoretical expansion engine 3P aiming at increased combustion of hydrogen + oxygen in FIG. 5 includes a repulsive permanent magnet 9B attracting permanent magnet 9C compressed air portion 9D vacuum portion 9E aiming at ultra-low cost rotation output such as ultra-large size and ultra-high speed rotation, and magnetic force + air pressure. By using the bearing load close to zero, the vertical turbine blades critical material gravity turbine 8N fuel cost 0 power generation Extremely cheap electricity production from electricity + liquid air cold heat + superheated steam temperature supply facility 3D, liquid oxygen 5K + electricity + superheat By receiving steam and compressing liquid oxygen 5K, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen 5K + liquid fuel 1c + water 52a is compressed to ultra high pressure such as 24-200 MPa. Then, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is heated to the optimum temperature on the inner wall of the open theoretical combustion chamber 4Y, and the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 2 b is opened, for example, the outer peripheral high-pressure high-temperature superheated steam 50 is heated by combustion at 3000 ° C. or more in the vicinity of a plurality of oxygen acetylene burners, and a part of the superheated steam 50 is aimed at the suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion near the center. As the superheated steam 50, fuel, and oxygen heated to the optimum temperature, the inner wall is subjected to protective combustion or ultra-high pressure / high temperature combustion, the combustion gas 49 is injected from the combustion gas injection nozzle 6Y, and the compressed intake air passage 5b of the air injection nozzle 5 Compressed air or intake air is sucked and injected, fuel injection combustion combustion amount is greatly increased from the fuel pipe 25c fuel injection nozzle 6X, and the theoretical expansion engine 3P is driven to increase the fuel combustion amount. 49 is injected 380 degrees in the circumferential direction from the center, and the upper expansion blade group 8d and the lower expansion blade group 8e are optimally injected horizontal axis 1h. The volume as the best theoretical expansion engine 3P in theory, which is inversely proportional to the pressure, the theoretical expansion engine 3P for injecting the turbine outer casing 77a assembled turbine blade group 8f.

図6の酸素合体水噴射部88Kのロケット燃焼+ジェット燃焼駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+過熱蒸気を受給して、液体酸素5Kを圧縮することで、圧縮容積仕事率を空気圧縮の21/60000容積圧縮仕事率にし、液体酸素5K+液体燃料1c+水52aを24〜200MPa等超高圧に圧縮して、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放、理論燃焼室4Y燃焼流内壁5d等で最適温度に加熱し、理論燃焼室4Yの過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放、例えば酸素アセチレンバーナー複数中心付近3000℃以上燃焼で外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、理論燃焼室4Y等燃焼流内壁5dの燃料加熱管1L+酸素加熱管5F+水加熱管5Hの燃料+酸素+水を加熱して、最適温度の過熱蒸気を外周に燃料+酸素複数中心付近ロケット燃焼とし、内壁の保護燃焼や超高圧高温ロケット燃焼噴射して、圧縮吸入空気路5b空気吸引流に燃料噴射ノズル6X燃料噴射ジェット燃焼にし、超高圧高温ロケット燃焼+ジェット燃焼1〜複数回として、先頭部複数過熱蒸気噴射ノズル6A噴射した外周200MPa狙い過熱蒸気50を加熱し、中心複数直列理論燃焼室4y外周等で次々過熱蒸気を加熱噴射推進出力を大増大して、ロケット燃焼+ジェット燃焼複数加速の燃焼ガス噴射ノズル6Y燃焼ガスを噴射し、200MPa噴射狙い過熱蒸気噴射ノズル6A超高速噴射して、内部燃焼ガス噴射ノズル6Yの燃焼ガス49と外周の前方空気28aを吸引噴射し、前方の水52aを吸引噴射する酸素合体水噴射部88Kにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Rocket combustion + jet combustion drive of oxygen combined water injection section 88K in FIG. 6 is a vertical type full blade ratio material gravity turbine 8N fuel cost 0 power generation extremely cheap electricity production of electricity + liquid air cold heat + superheated steam heat supply By receiving liquid oxygen 5K + electricity + superheated steam from the facility 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 volume compression work rate of air compression, and the liquid oxygen 5K + liquid fuel 1c + water 52a. Is compressed to an ultrahigh pressure such as 24 to 200 MPa, the liquid oxygen control valve 5T + the liquid fuel control valve 1K + the water control valve 5Q is opened, heated to the optimum temperature by the theoretical combustion chamber 4Y combustion flow inner wall 5d, etc. Open the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b. Heat, aim at a part of the superheated steam 50 near the center by suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion, fuel heating pipe 1L of combustion flow inner wall 5d such as theoretical combustion chamber 4Y + oxygen heating pipe 5F + fuel of water heating pipe 5H + Oxygen + water is heated, superheated steam at the optimum temperature is used as fuel + oxygen multi-center rocket combustion around the outer periphery, protective combustion of the inner wall and ultra high pressure high temperature rocket combustion injection are performed, and fuel is supplied to the compressed intake air passage 5b air suction flow Injecting nozzle 6X fuel injection jet combustion, super high pressure high temperature rocket combustion + jet combustion 1 to several times, heating the superheated steam 50 aiming at the outer peripheral 200MPa jet injected at the top multiple superheated steam injection nozzle 6A, the central multiple series theoretical combustion chamber 4y The superheated steam is heated one after another on the outer circumference, etc., and the jet propulsion output is greatly increased, and the rocket combustion + jet combustion multiple acceleration combustion gas injection nozzle 6Y combustion gas is injected, A superheated steam injection nozzle 6A aiming at 00 MPa injection is injected into the oxygen combined water injection section 88K that injects the combustion gas 49 of the internal combustion gas injection nozzle 6Y and the front air 28a on the outer periphery and sucks and injects the front water 52a. Various energy storage cycle coalescence engines and coalescence methods.

図7の酸素合体空気噴射部88Aのロケット燃焼+ジェット燃焼駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+過熱蒸気を受給して、液体酸素5Kを圧縮することで、圧縮容積仕事率を空気圧縮の21/60000容積圧縮仕事率にし、液体酸素5K+液体燃料1c+水52aを24〜200MPa等超高圧に圧縮して、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放、理論燃焼室4Y燃焼流内壁5d等で最適温度に加熱し、理論燃焼室4Yの過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放、例えば酸素アセチレンバーナー複数中心付近3000℃以上燃焼で外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、理論燃焼室4Y等燃焼流内壁5dの燃料加熱管1L+酸素加熱管5F+水加熱管5Hの燃料+酸素+水を加熱して、最適温度の過熱蒸気を外周に燃料+酸素複数中心付近ロケット燃焼とし、内壁の保護燃焼や超高圧高温ロケット燃焼噴射して、圧縮吸入空気路5b空気吸引流に燃料噴射ノズル6X燃料噴射ジェット燃焼にし、超高圧高温ロケット燃焼+ジェット燃焼1〜複数回として、先頭部複数過熱蒸気噴射ノズル6A噴射した外周200MPa狙い過熱蒸気50を加熱し、中心複数直列理論燃焼室4y外周等で次々過熱蒸気を加熱噴射推進出力を大増大して、ロケット燃焼+ジェット燃焼複数加速の燃焼ガス噴射ノズル6Y燃焼ガスを噴射し、200MPa噴射狙い過熱蒸気噴射ノズル6A超高速噴射して、内部燃焼ガス噴射ノズル6Yの燃焼ガス49と外周の前方空気28aを吸引噴射酸素合体空気噴射部88Aにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The rocket combustion + jet combustion drive of the oxygen coalesced air injection section 88A in FIG. 7 is a vertical all-blade ratio critical material gravity turbine 8N fuel cost 0 power generation extremely cheap electricity production of electricity + liquid air cold heat + superheated steam heat supply By receiving liquid oxygen 5K + electricity + superheated steam from the facility 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 volume compression work rate of air compression, and the liquid oxygen 5K + liquid fuel 1c + water 52a. Is compressed to an ultrahigh pressure such as 24 to 200 MPa, the liquid oxygen control valve 5T + the liquid fuel control valve 1K + the water control valve 5Q is opened, heated to the optimum temperature by the theoretical combustion chamber 4Y combustion flow inner wall 5d, etc. Open the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b, for example, combustion at 3000 ° C. or more in the vicinity of a plurality of centers of oxygen acetylene burner, high pressure high temperature superheated steam 50 Heat and aim at a part of the superheated steam 50 in the vicinity of the center to increase combustion by suction pyrolysis electrolysis oxygen hydrogen hydrogen, fuel heating pipe 1L of the combustion flow inner wall 5d such as the theoretical combustion chamber 4Y + fuel of the oxygen heating pipe 5F + water heating pipe 5H + Oxygen + water is heated, superheated steam at the optimum temperature is fueled on the outer periphery + rocket combustion near multiple oxygen centers, and protective combustion of the inner wall and super high pressure / high temperature rocket combustion injection are performed, and the compressed intake air passage 5b is in the air suction flow Fuel injection nozzle 6X Fuel injection jet combustion, super high pressure high temperature rocket combustion + jet combustion 1 to several times, the top superheated steam injection nozzle 6A injected superheated steam 50 is heated and the central multiple series theoretical combustion chamber 4y superheated steam one after the other on the outer circumference, etc., greatly increasing the injection propulsion output, rocket combustion + jet combustion multiple acceleration combustion gas injection nozzle 6Y combustion gas injection Superheated steam injection nozzle 6A aiming at 200 MPa injection, and a combination of various energy storage cycle coalescence engines and coalescence, with the combustion gas 49 of the internal combustion gas injection nozzle 6Y and the front air 28a on the outer periphery as a suction injection oxygen combination air injection unit 88A. To the way.

図8の水素+酸素増大燃焼狙う理論膨張機関3P理論燃焼室4Y自動車駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+過熱蒸気を受給して、液体酸素5Kを圧縮することで、圧縮容積仕事率を空気圧縮の21/60000容積圧縮仕事率にし、液体酸素制御弁5Tを開放液体酸素5Kをを液体酸素ポンプ4bで昇圧理論燃焼室4Y内壁に供給して、水制御弁5Q開放水52aを水ポンプ4cで昇圧理論燃焼室4Y内壁に供給し、液体燃料制御弁1K開放液体燃料1cを液体燃料ポンプ4aで昇圧理論燃焼室4Y内壁に供給して、最適温度に加熱+高圧高温過熱蒸気50製造し、図5過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放して、例えば酸素アセチレンバーナー複数中心付近3000℃以上の燃焼にし、外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、過熱蒸気50により理論燃焼室4Y内壁の液体酸素5K+液体燃料1c+水52aを加熱して、最適温度の過熱蒸気50や燃料や酸素や内壁の保護燃焼や超高圧高温燃焼にし、高圧高温燃焼ガス制御弁5aを開放理論膨張機関3Pを駆動して、発電機1を駆動して蓄電池1Aに蓄電して蓄電池駆動車輪4J駆動し、CO2排気1/10燃料費1/10運用利益率既存自動車の10倍狙う、理論膨張機関3P自動車にする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Fig. 8 Theoretical expansion engine 3P theoretical combustion chamber 4Y vehicle drive aiming at hydrogen + oxygen increase combustion in Fig. 8 is a vertical type moving blade ratio critical material gravity turbine 8N fuel cost 0 power generation extremely cheap electricity production of electricity + liquid air cold + superheat By receiving liquid oxygen 5K + electricity + superheated steam from the steam temperature heat supply equipment 3D and compressing the liquid oxygen 5K, the compression volume work rate is changed to 21/60000 volume compression work rate of air compression, and the liquid oxygen control valve 5T The open liquid oxygen 5K is supplied to the inner wall of the boosted theoretical combustion chamber 4Y by the liquid oxygen pump 4b, the water control valve 5Q is supplied to the inner wall of the boosted theoretical combustion chamber 4Y by the water pump 4c, and the liquid fuel control valve 1K is supplied. The open liquid fuel 1c is supplied to the inner wall of the boosted theoretical combustion chamber 4Y by the liquid fuel pump 4a, and heated to the optimum temperature + high-pressure high-temperature superheated steam 50 is manufactured, FIG. 5 superheated steam control valve 25 + oxygen control valve 24D + The charge control valve 25b is opened, for example, combustion is performed at 3000 ° C. or more in the vicinity of a plurality of centers of oxygen acetylene burners, the outer peripheral high-pressure high-temperature superheated steam 50 is heated, and a part of the superheated steam 50 is sucked pyrolytically electrolyzed oxygen near the center Aiming at increased hydrogen combustion, the superheated steam 50 heats the liquid oxygen 5K + liquid fuel 1c + water 52a on the inner wall of the theoretical combustion chamber 4Y to achieve the superheated steam 50, fuel, oxygen, inner wall protection combustion or ultrahigh pressure / high temperature combustion at the optimum temperature. The high-pressure high-temperature combustion gas control valve 5a is opened, the theoretical expansion engine 3P is driven, the generator 1 is driven, the storage battery 1A is charged, the storage battery drive wheel 4J is driven, and the CO2 exhaust 1/10 fuel cost 1/10 operation Profit rate Targeted 10 times that of existing automobiles, theoretical expansion engine 3P automobiles, various energy conservation cycle coalescence engines and coalescence methods.

図9酸素合体スクリュウ船舶39Hの、酸素水素増大燃焼狙う理論膨張機関3P理論燃焼室4Y駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5Kを受給電気+過熱蒸気を選択受給して、液体酸素5Kの理論燃焼室4Y燃焼高圧高温燃焼ガス制御弁5a開放理論膨張機関3P駆動は、液体酸素5Kを液体圧縮することで、圧縮容積仕事率を空気圧縮の21/60000容積圧縮仕事率にし、液体酸素5K+液体燃料1c+水52aを、液体燃料ポンプ4a+液体酸素ポンプ4b+水ポンプ4cで圧縮24〜200MPa等超高圧に圧縮して、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放、理論燃焼室4Y内壁等で最適温度に加熱し、図5過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放、例えば酸素アセチレンバーナー複数中心付近3000℃以上燃焼で外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、過熱蒸気50により理論燃焼室4Y内壁の液体酸素5K+液体燃料1c+水52aを加熱して、最適温度の過熱蒸気50や燃料や酸素や内壁の保護燃焼や超高圧高温燃焼にし、高圧高温燃焼ガス制御弁5aを開放理論膨張機関3P複数駆動を選択可能として、スクリュウ駆動して酸素合体スクリュウ船舶39Hを駆動し、CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、酸素合体スクリュウ船舶39Hにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Fig. 9 Oxygen combined screw ship 39H, theoretical expansion engine 3P theoretical combustion chamber 4Y driving aiming to increase combustion of oxygen and hydrogen, is a vertical all-blade ratio critical material gravity turbine 8N fuel cost 0 power generation extremely cheap electricity production of electricity + liquid The liquid oxygen 5K is received from the air cold heat + superheated steam temperature supply facility 3D, and the electricity + superheated steam is selectively received, and the theoretical combustion chamber 4Y combustion high pressure high temperature combustion gas control valve 5a driving of the liquid oxygen 5K is opened. By compressing liquid oxygen 5K into a liquid, the compression volume work rate is 21/60000 volume compression work of air compression, and liquid oxygen 5K + liquid fuel 1c + water 52a is compressed by liquid fuel pump 4a + liquid oxygen pump 4b + water pump 4c. Compressed to ultra-high pressure such as 24-200MPa, open the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q, optimal in the inner wall of the theoretical combustion chamber 4Y The superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b is opened, for example, the outer peripheral high-pressure high-temperature superheated steam 50 is heated by combustion at 3000 ° C. or more in the vicinity of a plurality of oxygen acetylene burner centers. A part of the heat is generated by suction pyrolysis electrolysis oxygen oxygen hydrogen combustion near the center, and the superheated steam 50 heats the liquid oxygen 5K + liquid fuel 1c + water 52a on the inner wall of the theoretical combustion chamber 4Y so Oxygen and inner wall protection combustion or ultra high pressure / high temperature combustion is performed, the high pressure / high temperature combustion gas control valve 5a can be selected to open a plurality of open theoretical expansion engines 3P, the screw is driven to drive the oxygen combined screw ship 39H, and the CO2 exhaust 1 / 10 Fuel Cost 1/10 Operating Profit Margin Various energy conservation cycle coalescence to make oxygen coalescence screw vessel 39H aiming 10 times of existing vessel To Seki and coalescence method.

図10酸素合体スクリュウ噴射船舶39Kの、酸素水素増大燃焼狙う理論燃焼室4Yによる酸素合体水噴射部88K理論膨張機関3P駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5Kを受給電気+過熱蒸気を選択受給して、理論膨張機関3Pによるスクリュウ駆動は図5横軸1h駆動や図9説明と同様駆動とし、酸素合体水噴射部88Kに理論燃焼室4Yを図6説明のように移動して、空気28a入口を前向き拡大して可能な限り直線に近付けた噴射推進として具備し、先頭理論燃焼室4Y燃焼ガス噴射ノズル6Y周囲には吸入空気路5bを具備して、ロケット燃焼にジェット燃焼追加船底に気泡最大噴射し、流線型理論燃焼室4Y1〜複数を用途に合わせて直列具備して、液体酸素5K圧縮で空気容積圧縮仕事率の21/60000容積圧縮仕事率にし、図6の流線型理論燃焼室4Yは用途に合せて1〜複数使用して、200MPa狙い過熱蒸気噴射で燃焼ガス+前方の空気を吸引噴射し、水を吸引噴射して、噴射推進する大型船舶や小型船舶や高速船舶や超高速船舶にし、ロケット燃焼にジェット燃焼追加した燃焼量増大にして、酸素合体水噴射部88K超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、酸素合体水噴射部88Kにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 FIG. 10 Oxygen combined screw injection vessel 39K, oxygen combined water injection unit 88K theoretical expansion engine 3P driven by theoretical combustion chamber 4Y aiming at increased oxygen hydrogen combustion, vertical type full blade ratio material gravity turbine 8N fuel cost 0 power generation extreme The screw drive by the theoretical expansion engine 3P by receiving the liquid oxygen 5K from the electricity + liquid air cold heat + superheated steam temperature supply facility 3D, which is a low-cost electric manufacture, and selectively receiving the superheated steam 3P is shown in FIG. 9 is driven as in the explanation, the theoretical combustion chamber 4Y is moved to the oxygen coalescence water injection section 88K as shown in FIG. 6 and the inlet of the air 28a is expanded forward to be as close to a straight line as possible, The leading theoretical combustion chamber 4Y is provided with an intake air passage 5b around the combustion gas injection nozzle 6Y, and the maximum bubble injection is performed on the bottom of the jet combustion additional vessel for rocket combustion, and the streamline theoretical combustion chamber 4Y1 A plurality of units are provided in series according to the application, and the liquid oxygen 5K compression is set to 21/60000 volumetric compression power of the air volumetric compression power. The streamlined theoretical combustion chamber 4Y in FIG. , Combustion gas with superheated steam injection aiming at 200 MPa, sucking and injecting combustion gas + air in front, sucking and injecting water to make large and small vessels, high-speed vessels and ultra-high-speed vessels propelling injection, jet combustion added to rocket combustion Oxygen combined water injection part 88K super high pressure mass combustion 100 times output target, 10% speed target injection propulsion of existing ship, same speed CO2 exhaust 1/10 fuel cost 1/10 operation profit rate existing ship The oxygen coalescence water injection unit 88K is aimed at 10 times the energy storage cycle coalescence engine and the coalescence method.

図11酸素合体噴射船舶39Jの、酸素水素増大燃焼狙う理論燃焼室4Yによる酸素合体水噴射部88K駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5Kを受給電気+過熱蒸気を選択受給して、酸素合体水噴射部88Kに理論燃焼室4Yを図6説明のように具備し、先頭理論燃焼室4Y燃焼ガス噴射ノズル6Y周囲には吸入空気路5bを具備して、燃料噴射ノズル6X複数より吸入空気等に燃料噴射燃焼し、ジェット燃焼追加する図6流線型理論燃焼室4Y1〜複数を用途に合わせて選択具備として、液体酸素5K圧縮で空気容積圧縮仕事率の21/60000容積圧縮仕事率にし、200MPa狙い過熱蒸気噴射で燃焼ガス+空気を吸引噴射+前方の水を吸引噴射して、噴射推進する大型船舶や小型船舶や高速船舶や超高速船舶にし、ロケット燃焼にジェット燃焼追加した燃焼量増大にして、酸素合体水噴射部88K超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、酸素合体水噴射部88Kにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 FIG. 11 The oxygen coalescence water injection unit 88K driven by the theoretical combustion chamber 4Y of the oxygen coalescence injection ship 39J aiming at increased oxygen-hydrogen combustion is a vertical all-blade ratio critical material gravity turbine 8N fuel cost 0 power generation extremely cheap electric production, Electricity + liquid air cold heat + superheated steam temperature supply equipment 3D receives liquid oxygen 5K, selectively receives electricity + superheated steam, and comprises a theoretical combustion chamber 4Y in the oxygen combined water injection unit 88K as illustrated in FIG. The leading theoretical combustion chamber 4Y is provided with an intake air passage 5b around the combustion gas injection nozzle 6Y. The fuel injection nozzle 6X injects fuel into the intake air and the like, and adds jet combustion. Is selected according to the application, liquid oxygen 5K compression is 21/60000 volumetric compression work rate of air volumetric compression work rate, combustion gas + air is aimed at 200MPa with superheated steam injection Pulling injection + sucking and jetting forward water to make large and small vessels, high-speed vessels and ultra-high-speed vessels propelled by injection, increasing the combustion amount by adding jet combustion to rocket combustion, oxygen combined water injection part 88K super high pressure Assuming that the mass combustion is 100 times the output, the injection speed is 10 times that of the existing ship, and the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate is 10 times that of the existing ship. And various energy storage cycle coalescence engines and coalescence methods.

図12酸素合体噴射飛行機39Lの、酸素水素増大燃焼狙う理論燃焼室4Yによる酸素合体空気噴射部88A駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5Kを受給電気+過熱蒸気を選択受給して、酸素合体空気噴射部88Aに理論燃焼室4Yを図7のように具備し、先頭理論燃焼室4Y燃焼ガス噴射ノズル6Y周囲には吸入空気路5b複数具備して、ロケット燃焼にジェット燃焼追加する流線型理論燃焼室4Y1〜複数を用途に合わせて具備し、液体酸素5K圧縮で空気容積圧縮仕事率の21/60000容積圧縮仕事率にして、図7のロケット燃焼+ジェット燃焼で噴射推進し、宇宙上昇時にはロケット燃焼により宇宙に到達する宇宙往還の各種飛行機にして、酸素合体空気噴射部88A超高圧大量燃焼100倍出力狙いとし、燃料費0に近い宇宙利用全盛1日に地球を16周する等地球上何処でも日帰り旅行を可能にして、大気中同一速度CO2排気1/10燃料費1/10運用利益率既存飛行機の10倍狙う、酸素合体空気噴射部88Aにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 FIG. 12 Oxygen combined injection plane 39L of oxygen combined air injection unit 88A driven by theoretical combustion chamber 4Y aiming at increased combustion of oxygen and hydrogen is vertical full blade ratio material gravity turbine 8N fuel cost 0 power generation Electricity + liquid air cold heat + superheated steam temperature supply equipment 3D receives liquid oxygen 5K, selectively receives electricity + superheated steam, the oxygen combined air injection section 88A has a theoretical combustion chamber 4Y as shown in FIG. Theoretical combustion chamber 4Y is provided with a plurality of intake air passages 5b around the combustion gas injection nozzle 6Y, and is equipped with a plurality of streamlined theoretical combustion chambers 4Y1 to 4 for adding jet combustion to rocket combustion in accordance with the application, and an air volume by liquid oxygen 5K compression The compression work rate is set to 21/60000 volumetric compression work rate, propelled by rocket combustion + jet combustion shown in FIG. 7, and reaches the universe by rocket combustion when the space rises. It is possible to make day trips anywhere on the earth, such as making 16 rounds of the earth in a space use prime day near the fuel cost of 0, aiming at 100 times output of oxygen combined air injection part 88A ultra high pressure mass combustion as various airplanes in the air In the atmosphere, CO2 exhaust 1/10 fuel cost 1/10 operating profit ratio The oxygen coalescence air injection unit 88A aiming 10 times that of the existing airplane is made into various energy storage cycle coalescence engines and coalescence methods.

図13酸素合体プロペラ飛行機39Mの、酸素水素増大燃焼狙う図5理論燃焼室4Y理論膨張機関3Pプロペラ7A駆動は、竪型全動翼比重大物質重力タービン8N燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから、液体酸素5Kを受給電気+過熱蒸気を選択受給して、圧縮24〜200MPa等とし、液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放して、理論燃焼室4Y内壁等で最適温度に加熱し、過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放、例えば酸素アセチレンバーナー複数中心付近3000℃以上燃焼で外周高圧高温過熱蒸気50を加熱して、過熱蒸気50の一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙いにし、過熱蒸気50により理論燃焼室4Y内壁等の液体酸素5K+液体燃料1c+水52aを加熱して、最適温度の過熱蒸気50や燃料や酸素や内壁の保護燃焼や超高圧高温燃焼にし、燃焼ガス噴射ノズル6Y中心より380度外周方向噴射で理論膨張機関3P駆動して、横軸1hによりプロペラ7A駆動や回転翼7B駆動にし、大気中同一速度CO2排気1/10燃料費1/10運用利益率既存飛行機の10倍狙う、プロペラ飛行機等にし図12と合体酸素合体プロペラ噴射飛行機39Nにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Fig. 13 Oxygen combined propeller plane 39M, aiming at increased oxygen hydrogen combustion Fig. 5 Theoretical combustion chamber 4Y Theoretical expansion engine 3P propeller 7A drive is a vertical all-blade ratio critical material gravity turbine 8N fuel cost 0 power generation extremely cheap electricity production , Electricity + liquid air cold heat + superheated steam temperature supply facility 3D receives liquid oxygen 5K, selectively receives electricity + superheated steam, compresses to 24 to 200 MPa, etc., liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened and heated to the optimum temperature on the inner wall of the theoretical combustion chamber 4Y, etc., and the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b is opened. The superheated steam 50 is heated, and a part of the superheated steam 50 is aimed at increasing the suction pyrolysis electrolysis oxygen-hydrogen hydrogen combustion near the center. Liquid oxygen 5K + liquid fuel 1c + water 52a on the inner wall of the combustion chamber 4Y and the like are heated to produce superheated steam 50, fuel, oxygen, inner wall protection combustion and super high pressure high temperature combustion at the optimum temperature, and 380 degrees from the center of the combustion gas injection nozzle 6Y. The theoretical expansion engine 3P is driven by the peripheral direction injection, and the propeller 7A drive and the rotor blade 7B drive are driven by the horizontal axis 1h, and the same speed CO2 exhaust in the atmosphere 1/10 fuel cost 1/10 operating profit rate Aim 10 times the existing airplane, Various energy storage cycle merging engines and merging methods, such as a propeller airplane or the like, are combined with the oxygen merging propeller injection airplane 39N shown in FIG.

資源価格0燃料費0発電の原価を原子力発電の1/2以下狙う、竪型全動翼比重大物質重力タービン8N発電を既存揚水発電と比較説明すると、揚水発電の発電部分に、真空中の重力加速度とウォータージェット加工機の水噴射速度マッハ3を追加し、仕事率が速度に比例+高さに比例+10倍速度1/10容積垂直水銀駆動+全動翼横軸1h二重反転駆動で、真空中重力加速度9.8m/秒の威力を最大として、世界最高建築物高さ828mに200組垂直具備で1台発電とし、既存揚水発電と同一水銀量2710倍発電量等の竪型全動翼比重大物質重力タービン8N発電で、極端に安価発電にする可能性がある。 Compared to the existing pumped-storage power generation, the vertical-type moving blade ratio critical material gravity turbine 8N power generation aiming at a resource price of 0 fuel costs of 0 power generation less than 1/2 of the nuclear power generation. Gravity acceleration and water jet processing machine water jet speed Mach 3 are added, work rate is proportional to speed + proportional to height + 10 times speed 1/10 volume vertical mercury drive + all blade horizontal axis 1h with double reversal drive , With a maximum of 9.8m / sec in gravity acceleration in vacuum, 200 units vertically installed in the world's highest building height of 828m, and one unit of power generation, the same mercury amount as the existing pumped storage power generation 2710 times the total amount of power generation, etc. There is a possibility of extremely low cost power generation by gravity turbine 8N power generation.

資源価格0燃料費0発電の原価を原子力発電の1/2以下狙う、竪型全動翼比重大物質重力タービン8N発電を既存火力原子力蒸気タービン発電と比較説明の過程で、ボイルの法則により大気圧100℃760mmHgで水の1700倍容積の水蒸気は、排気温度29℃真空度30mmHg蒸気圧で水の43000倍容積水蒸気となり、既存蒸気タービン最終動翼群蒸気速度を音速と仮定すると、入口高圧動翼群蒸気速度は音速の1/100速度以下仕事率最低のため、最高仕事率の最終動翼群と比較説明する。水の駆動容積が水蒸気29℃容積の1/43000容積29℃水駆動の場合、全動翼横軸1h二重反転する6段前後動翼群駆動で同発電量となり、1/215容積水駆動で200倍発電量200組連結の1台で40000倍発電量となり、水銀駆動で542000倍発電量となる等、小学校理科で計算すると極端に安価発電を天文学的大発電量にする可能性がある。 Aiming to reduce the cost of resource 0 fuel cost 0 power generation to less than 1/2 of nuclear power generation, the vertical type blade blade critical material gravity turbine 8N power generation is compared with the existing thermal power nuclear steam turbine power generation by Boyle's law. Assuming that the steam velocity of 1700 times the water at an atmospheric pressure of 100 ° C. and 760 mmHg becomes 43,000 times the volume of water at an exhaust temperature of 29 ° C. and a vacuum degree of 30 mmHg and the steam velocity of the final moving blade group of the existing steam turbine is sonic, Since the blade group vapor velocity is 1 / 100th the speed of sound or less and the work rate is the lowest, the comparison will be made with the last blade group having the highest work rate. When the water drive volume is 1/43000 volume 29 ° C water drive of the steam 29 ° C volume, the same power generation amount is obtained by driving the 6-stage front and rear blade groups that are double-reversed for 1 h for all the rotor blades. With 200 units of power generation 200 units connected, the power generation amount is 40,000 times, and mercury-driven power generation amount is 542,000 times. If calculated by elementary school science, there is a possibility of making cheap power generation extremely large astronomical power generation. .

竪型全動翼比重大物質重力タービン8N発電極端に安価発電の、電気製造物全盛として電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより過熱蒸気を受給して、海底や永久凍土地下のメタンハイドレートに注入囲い設けてメタン回収や永久凍土地帯の牧草地放牧変換や、オイルサンド地帯やオイルシェール地帯や老朽石油採取地帯でも過熱蒸気注入し、夫々囲い設けて気化回収液化保存等として、食品会社では過熱蒸気安価受給して安価食料品大量製造等とし、農業用や工業用や産業用や鉱業用に使用して温熱利用全盛にする可能性がある。 Vertical type moving blade ratio critical material gravity turbine 8N power generation Extremely inexpensive power generation as an electric product prime, electricity + liquid air cold heat + superheated steam temperature supply facility 3D receives superheated steam, methane under the seabed and permafrost land Injecting enclosures in hydrates to collect methane, conversion to pasture grazing in permafrost, superheated steam injection in oil sands, oil shales, and old oil extraction areas, respectively, to provide vaporization, recovery, liquefaction, etc. A company may receive superheated steam at low cost for mass production of low-priced foods, etc., and use it for agriculture, industrial use, industrial use, mining, etc.

竪型全動翼比重大物質重力タービン8N発電極端に安価発電の、電気製造物全盛として電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより液体酸素5Kを受給して、液体酸素で駆動する自動車や船舶や飛行機等とし、液体酸素5Kを液体圧縮することで空気容積圧縮仕事率の21/60000容積圧縮仕事率にして、理論膨張機関3Pや酸素合体水噴射部88Kや酸素合体空気噴射部88Aを駆動し、自動車ではCO2排気や燃料費を1/10に近付ける可能性があり、船舶は同一燃料費で10倍速度に近付ける可能性があり、飛行機は宇宙到達費用を1/50万等として、宇宙利用全盛として地球上何処でも日帰り旅行にする等、冷熱利用全盛の大革命にする可能性がある。 Vertical type moving blade ratio critical material gravity turbine 8N power generation Extremely inexpensive power generation, electric product prime as an electric + liquid air cold heat + superheated steam temperature supply equipment 3D receives liquid oxygen 5K, driven by liquid oxygen Or a ship, an airplane, etc., by liquid compressing liquid oxygen 5K to 21/50000 volume compression work rate of air volume compression work rate, theoretical expansion engine 3P, oxygen combined water injection unit 88K, oxygen combined air injection unit 88A There is a possibility that CO2 emissions and fuel costs will be close to 1/10 in automobiles, ships may be close to 10 times the speed with the same fuel cost, and airplanes will have a space arrival cost of 1 / 500,000, etc. There is a possibility that it will be a major revolution in the use of cold energy, such as making a day trip anywhere on earth as a prime use of space.

0:各種エネルギ保存サイクル合体機関(各種熱エネルギは空気温度として熱ポンプで圧縮熱回収して、液体空気冷熱+過熱蒸気温熱に分割保存使用、重力エネルギは上昇保存噴射真空中重力加速度加速して発電電力に変換使用する各種エネルギ合体エンジン合体手段) 0:各種エネルギ保存サイクル合体機関及び合体方法(各種熱エネルギは太陽熱や地熱で加熱等空気温度として熱ポンプで圧縮熱回収して、液体空気冷熱+過熱蒸気温熱に分割保存使用・500℃以下液体金属使用時は保温装置で保温保存使用・衝撃エネルギはタービン翼や小径金属球にし、シリコン樹脂被覆やフッ素樹脂被覆を設け作用時間の保存延長に使用・重力エネルギは上昇装置により上昇保存噴射真空中重力加速度加速して発電電力で変換使用する各種エネルギ合体エンジン及び各種エネルギ合体手段) 1:発電機、 1A:蓄電池、 1B:圧力機関(酸素圧力歯車機関・酸素圧力往復機関・水圧力歯車機関・水圧力往復機関等液体圧縮で圧縮仕事率を1/600として圧縮機やポンプを各種圧力機関にする) 1C:アルコール、 1D:燃料噴射ポンプ、 1F:復水ポンプ、 1G:1〜複数段熱ポンプ(熱エネルギを空気温度とし熱ポンプ(各種空気圧縮機)で複数回圧縮2Cの2X2Y2Zで複数回熱回収温熱50+冷熱28aで分割保存) 1K:液体燃料制御弁、 1L:燃料加熱管、 1Y:複数段燃焼室(液体酸素と液体窒素を別圧縮50〜200MPa燃焼ガスと窒素ガス別製造し、1Yに燃焼ガス噴射燃料噴射燃焼内外の水蒸気加熱を複数回実施して噴射又は排気する) 1b:燃料(液体燃料+液化可能気体燃料) 1b:燃料管(燃料噴射温度が最適温度になるように具備する) 1c:液体燃料、 1d:水銀、 1g:重力加速部、 1h:横軸(外側軸装置と内側軸装置の回転方向交互にする軸) 2:太陽光加熱器(長レンズで太陽光を直線状に集めて高温部形成吸入空気を加熱) 2a:自然現象高速化(空気中では変化略0の残飯類が近くの川に移動すると一夜で0に近付く膨大な微生物量を人類の食糧増大に利用) 2a:自然現象高速化(発電では海水に冷熱28aを混合自然現象高速化した海水を海底に供給窒素や酸素やCO2等の栄養分を供給微生物増大して魚類やコンブ等食糧大増大する装置) 2a:自然現象高速化(船舶では海中に窒素や酸素やCO2等の栄養分を供給微生物の消化能力を森林の数万倍狙い植物プランクトンや海草等を増殖食物連鎖等により魚類やコンブ類等人類の食糧を増大) 2b:水抵抗僅少(船底に空気+燃焼ガス+過熱蒸気を超高速噴射して水抵抗僅少にする) 2c:断熱材、 2d:長レンズ(凸レンズ断面を直線状に延長矩形とし、複数使用で焦点距離最短レンズ幅最大狙う) 2e:水面、 2g:比重大物質加速方向、 2A:耐熱材、 2B:熱吸収材、 2C:1〜複数段圧縮熱回収器(熱エネルギを空気温度とし熱ポンプで複数回圧縮2Cの2X2Y2Z等各種熱交換器で複数回熱回収利用して残りを温熱50+液体冷熱28aに分割保存) 2E:比重大物質(合金含む、白金球・金球・タングステン合金粉末焼結球・銀球・銅球・錫球・鉛球・亜鉛球・アルミニウム球・インジウム・カドミウム・ガリウム・タリウム・ビスマス等比重の大きい物質) 2E:比重大物質(製造法は小径程衝撃エネルギが低減するため例えば溶融鋼を空気中に噴射高速衝突粉砕空気冷却水冷却で超小径鋼球等製造) 2E:比重大物質(シリコン樹脂被覆やケイ素樹脂被覆の、被覆白金合金球・被覆金合金球・被覆タングステン合金粉末焼結球・被覆銀合金球・被覆ビスマス合金球・被覆銅合金球・被覆錫合金球・被覆鉛合金球・被覆亜鉛合金球・被覆アルミニウム合金球) 2F:比重大物質上昇装置(重力エネルギを上昇保存) 2H:冷熱海水混合器(海水に冷熱を混合自然現象高速化の過程で過熱蒸気気化熱を冷却復水にする装置) 2X:空気熱交換器(空気を熱ポンプで圧縮高温として熱回収圧縮空気質量無限増大や圧力無限上昇狙う) 2Y:圧縮空気熱交換器(高温空気や燃焼ガスで空気冷熱+過熱蒸気温熱製造する) 2Z:比重大物質熱交換器(500度以下液体金属の温度管理等で使用) 3a:撥水鍍金、 3A:撥水コーティング、 3D:電気+液体空気冷熱+過熱蒸気温熱供給設備(重力発電電気で冷熱+温熱製造し、液体酸素や液体窒素を供給自動車や船舶や飛行機を駆動や過熱蒸気で供給メタンハイドレートに注入メタンを回収等電気+冷熱+温熱利用全盛にする) 3E:比重大物質(水銀や水等常温で液体の比重大物質) 3E:比重大物質(低融点合金の500度以下液体で安定高温液体合金) 3F:酸素圧力往復機関(液体酸素と液体窒素と燃料を噴射燃焼50〜200MPa燃焼ガスとし、膨張の過程で燃料噴射多段燃焼して多段酸素圧力往復機関を駆動する) 3G:理論燃焼歯車機関(液体酸素+液体燃料+水を圧縮加熱して噴射燃焼する) 3H:往復ピストン、 3J:理論燃焼往復機関(液体酸素+液体燃料+水を圧縮加熱して噴射燃焼する) 3K:外接歯車 3L:複数段燃焼室、 3M:水蒸気圧力往復機関(多段酸素圧力往復機関で水や水蒸気を多段加熱して多段水蒸気圧力往復機関を駆動する) 3N:水蒸気圧力歯車機関(多段酸素圧力歯車機関で水や水蒸気を多段加熱して多段水蒸気圧力歯車機関を駆動する) 3P:理論膨張機関(ボイルの法則気体の体積は圧力に反比例する理論で最良機関) 3R:理論ガスタービン(気体の体積は圧力に反比例対応の理論最良ガスタービン) 3S:理論蒸気タービン(気体の体積は圧力に反比例対応の理論最良蒸気タービン) 3T:理論気体圧縮機(気体の体積は圧力に反比例対応の理論最良気体圧縮機) 3U:理論タービン、 3V:ポンプ機関(既存各種ポンプをエンジンで使用) 3X:圧縮機機関(既存各種圧縮機をエンジンで使用) 3Y:二重反転機関(気体の体積は圧力に反比例対応のエンジン) 3Z:酸素圧力歯車機関(液体酸素と液体窒素と燃料噴射燃焼して50〜200MPa燃焼ガスとし内周外周の水や水蒸気を多段燃焼加熱して多段水蒸気圧力歯車機関を連動する) 3a:撥水鍍金、 3b:撥水コーティング、 4F:燃焼ガス往復機関、 4H:熱吸収管(長レンズ2dで太陽光を熱吸収管に直線状に集めて管内空気温度を最高に加熱して菅外空気温度も上昇する) 4J:蓄電池駆動車輪、 4K:理論膨張機関自動車、 4W:理論圧縮室、 4Y:理論燃焼室(水蒸気の中で高温燃焼して水の熱分解電気分解燃焼狙い化合物0狙い燃焼室) 4Z:燃焼ガス歯車機関、 4X:タービン翼断面(断面積を拡大表面積増大) 4a:液体燃料ポンプ、 4b:液体酸素ポンプ、 4c:水ポンプ、 4d:歯車装置、 4e:ローラー、 4f:回転支持部、 5:空気噴射ノズル、 5a:高圧高温燃焼ガス制御弁、 5b:圧縮吸入空気路、 5d:燃焼流内壁、 5e:超高圧酸素、 5A:給気弁、 5B:冷却ヒレ、 5C:排気室、 5D:排気弁、 5E:給気室、 5F:酸素加熱管、 5G:水蒸気加熱管、 5H:水加熱管、 5K:液体酸素、 5K:液体酸素室、 5L:液体窒素、 5L:液体窒素室、 5M:高圧高温燃焼ガス、 5M:高圧高温燃焼ガス室、 5N:高圧高温水蒸気室、 5N:高圧高温水蒸気、 5P:水蒸気制御弁、 5Q:水制御弁、 5R:過熱蒸気制御弁、 5S:圧縮空気加熱管、 5T:液体酸素制御弁、 6:最終圧縮翼、 6A:過熱蒸気噴射ノズル、 6B:圧縮空気噴射ノズル、 6C:燃焼ガス水蒸気ノズル、 6E:比重大物質噴射ノズル、 6F:水噴射ノズル、 6G:静翼、 6H:排水管、 6L:酸素噴射ノズル、 6W:比重大物質加速機(液体比重大物質3E圧力と比重差利用して比重大物質3Eや2E混合噴射) 6X:燃料噴射ノズル、6X:アフターバーナー(吸引空気流に燃料噴射冷熱28a燃焼流6Yに合流燃焼して燃料燃焼量大増大で宇宙上昇) 6Y:燃焼ガス噴射ノズル(冷熱28a燃焼流) 6Z:水蒸気噴射ノズル、 7A:プロペラ、 7B:回転翼、 7C:スクリュー、 8c:タービン翼(内側と外側動翼群夫々を内側と外側軸装置の円筒部に夫々嵌合組立固定する全自動製造加工狙うタービン翼) 8d:上側膨張翼群、 8e:下側膨張翼群、 8f:組立タービン翼群、 8g:上側圧縮翼群、 8h:下側圧縮翼群、 8j:組立圧縮翼群、 8H:竪型全動翼タービン(小型大出力段落毎環状同径略同形略同長ねじ組立9回転止め固定として互いに反対方向に回転する全動翼必須に対応し、軽量化等実験最良に移行) 8H:竪型全動翼タービン(超硬合金貼付やシリコン樹脂被覆やフッ素樹脂被覆のタービン翼選択) 8H:竪型全動翼水重力タービン(既存蒸気タービンは静翼で堰き止め出力が0に近付くため全動翼を必須とし、仕事率が白金球の1/3.6万等僅少なため比重大物質重力使用必須とし、太陽光加熱空気等空気を1〜複数段熱ポンプ+圧縮熱回収器で圧縮熱回収し、温熱+冷熱に分割保存タービン駆動+各種用途に使用) 8H:竪型全動翼水重力タービン(温熱駆動+冷熱駆動にすると使用落差が限定されるため落差使用無制限の場合使用) 8K:竪型全動翼水重力タービン(横軸1hにより外側軸装置と内側軸装置の回転方向交互にする水重力タービン) 8L:竪型全動翼比重大物質重力タービン(横軸1hにより外側軸装置と内側軸装置の回転方向交互にする比重大物質重力タービン) 8M:竪型全動翼水重力タービン(内側動翼群外側動翼群に円筒部を設けて加工容易組み立て容易軽量化容易にする) 8N:竪型全動翼比重大物質重力タービン(内側動翼群外側動翼群に円筒部を設けて加工容易組み立て容易軽量化容易にする) 9:耐摩耗環状組立(8cを含む比重大物質流路のみ超硬合金で環状製造軽量化する嵌合組立方法) 9A:円筒環状組立(耐摩耗円筒環状組立て動翼群6種類にすることで構造簡単や部品数僅少や全自動加工容易や組立容易や軽量化容易等にする) 9A:円筒環状組立(入口固定外翼60E+外側環状翼60G+出口固定外翼60J嵌合で円筒外側動翼群60Dを構成し、入口固定内翼60F+内側環状翼60H+出口固定内翼60K嵌合で円筒内側動翼群60Cを構成する円筒部) 9B:反発永久磁石、 9C:吸引永久磁石、 9D:圧縮空気部、 9E:真空部、 10:船体、 10A:船室、 10b:操縦室、 10c:制御室、 10d:客室、 10e:貨物室、 11D:気体専用冷却室、 16B:垂直軸、 21:太陽光加熱器(吸入空気路を熱吸収管4H内にも設けて主使用する) 24:燃焼ガス制御弁、 24A:圧縮空気制御弁、 24B:液体酸素制御弁、 24C:液体窒素制御弁、 24D:酸素制御弁、 24E:窒素制御弁、 25:過熱蒸気制御弁、 25b:燃料制御弁、 25c:燃料管、 28a:空気、 28a:冷熱(空気28aを熱ポンプで圧縮して圧縮空気熱量の過熱蒸気50温熱+液体酸素や液体窒素を含む圧縮空気28a冷熱に分割保存) 28b:圧縮空気熱量、 28A:吸入空気路、 28B:空気路入口、 38:回転案内具、 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、 38B:空気吸引噴射船舶(79S79T79Y79Z具備) 38C:水吸引噴射船舶(79U79X具備) 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、 39H:酸素合体スクリュー船舶、 39J:酸素合体噴射船舶、 39K:酸素合体スクリュー噴射船舶、 39L:酸素合体噴射飛行機、 39M:酸素合体プロペラ飛行機、 39N:酸素合体プロペラ噴射飛行機、 39P:酸素合体回転翼飛行機、 40A:方向舵、 49:燃焼ガス、 50:過熱蒸気、 50:過熱蒸気室、 50:温熱(空気28aを熱ポンプで圧縮して圧縮空気熱量の過熱蒸気50温熱+圧縮空気28a冷熱に分割保存) 50A:水蒸気、 50a:過熱蒸気噴射管、 51:空気抽出器、 5
1:合流抽出器(合流するための抽出器) 51A:空気抽出室、 52a:水、 52a:海洋深層水、 52b:高温水、 52d:温熱(50から変化) 52e:冷熱(28aから変化) 55B:変速装置、 60A:内側軸装置(タービン翼具備装置) 60B:外側軸装置(タービン翼具備装置) 60C:円筒内側動翼群(耐摩耗円筒環状組立固定動翼群を含めて全自動加工容易組立容易にする) 60D:円筒外側動翼群(耐摩耗円筒環状組立固定動翼群を含めて全自動加工容易組立容易にする) 60E:入口固定外翼(外側動翼群を環状組立固定する入口翼) 60F:入口固定内翼(内側動翼群を環状組立固定する入口翼) 60G:外側環状翼(外側動翼群を環状組立する中間翼) 60H:内側環状翼(内側動翼群を環状組立する中間翼) 60J:出口固定外翼(外側動翼群を環状組立固定する出口翼) 60K:出口固定内翼(内側動翼群を環状組立固定する出口翼) 76:歯車装置(磁気摩擦動力伝達装置を含む) 77B:半筒形外箱、 77F:噴射部外箱、 77G:円筒回転部、 77a:タービン外箱、 80:軸受(磁気軸受+空気軸受含) 80a:推力軸受(磁気軸受+空気軸受含) 80A:継手、 80B:締付具、 80E:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 80F:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 80V:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 80W:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 80S:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 80T:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 80U:液体水吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 80X:液体水吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 80Y:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 80Z:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 84:二重反転磁気摩擦装置(固定部具備内側動翼群と外側動翼群を略同速度反対回転にする装置) 84Y:二重反転歯車装置(既存技術で二重反転する装置) 85:二重反転磁気装置(磁石利用歯車高さ僅少から無接触にし横軸1h歯車により相互逆回転にする) 85Y:二重反転歯車装置(既存横軸1h歯車により相互逆回転にする) 88A:酸素合体空気噴射部(ロケット燃焼+ジェット燃焼+水蒸気噴射等と合体噴射) 88K:酸素合体水噴射部(ロケット燃焼+ジェット燃焼+水蒸気噴射等と合体噴射) 95a:燃焼ガス溜、 95b:圧縮空気溜、 95c:過熱蒸気溜、 103:冷熱回収器、
0: Various energy storage cycle coalesced engine (various heat energy is compressed and recovered by heat pump as air temperature, divided into liquid air cold heat + superheated steam heat, and gravitational energy is increased storage spray accelerated by acceleration of gravity in vacuum Various energy coalescence engine coalescence means used for conversion to generated power) 0: Various energy storage cycle coalescence engine and coalescence method (various thermal energy is heated by solar heat or geothermal heat, etc., compressed air is recovered by a heat pump as air temperature, liquid air cooling + Divided and stored in superheated steam temperature ・ Used with a heat retaining device when using liquid metal below 500 ℃ ・ Shock energy is set to turbine blades and small-diameter metal balls, and silicon resin coating or fluororesin coating is provided to extend the working time Use / gravity energy is ascended by the ascending device, stored and sprayed, accelerated by gravitational acceleration in vacuum, and converted into energy using generated power Combined engine and various energy combining means) 1: generator, 1A: storage battery, 1B: pressure engine (oxygen pressure gear engine, oxygen pressure reciprocating engine, water pressure gear engine, water pressure reciprocating engine, etc.) 1C: alcohol, 1D: fuel injection pump, 1F: condensate pump, 1G: 1 to multistage heat pump (heat pump with heat energy as air temperature (various air (Compressor) Multiple times compression 2C 2X2Y2Z 2X2Y2Z Multiple times heat recovery heat 50 + Cold 28a) 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Y: Multiple stage combustion chamber (Separate liquid oxygen and liquid nitrogen Compressed 50 to 200 MPa Combustion gas and nitrogen gas are manufactured separately, and 1Y is subjected to water vapor heating inside and outside the combustion gas injection multiple times to inject or exhaust) 1b: Fuel (liquid 1b: Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity acceleration unit, 1h: Horizontal axis (outer shaft device and inner side) 2) Sunlight heater (collects sunlight in a straight line with a long lens and heats the high-temperature portion forming intake air) 2a: Speeds up the natural phenomenon (change in air is almost zero) When the leftovers move to a nearby river, a huge amount of microorganisms that approaches zero overnight will be used to increase food for humans. Equipment that increases the supply of nutrients such as nitrogen, oxygen, and CO2 and increases foods such as fish and kombu. 2a: Speeds up natural phenomena (in ships, the supply of nutrients such as nitrogen, oxygen, and CO2 into the sea makes it possible to digest microorganisms. Planting aiming tens of thousands times the forest 2b: Low water resistance (lowly sprays air + combustion gas + superheated steam to the bottom of the ship to minimize water resistance) 2c : Insulating material, 2d: Long lens (Convex lens cross section linearly extended rectangle, multiple lenses are used to aim the maximum focal length shortest lens width) 2e: Water surface, 2g: Specific material acceleration direction, 2A: Heat-resistant material, 2B: Heat Absorbent, 2C: 1 to multi-stage compression heat recovery device (heat energy is air temperature, compression multiple times with heat pump, heat recovery is used multiple times with various heat exchangers such as 2C2X2Y2Z of 2C, and the rest is heated 50 + liquid cold 28a 2E: Specific critical substances (including alloys, platinum balls, gold balls, tungsten alloy powder sintered balls, silver balls, copper balls, tin balls, lead balls, zinc balls, aluminum balls, indium, cadmium, gallium, and tari 2E: Specific critical material (Manufacturing method reduces the impact energy as the diameter decreases. For example, molten steel is injected into the air to produce ultra-small diameter steel balls by high-speed collision pulverization air cooling water cooling) 2E : Specific critical materials (coated platinum alloy balls, coated gold alloy balls, coated tungsten alloy powder sintered balls, coated silver alloy balls, coated bismuth alloy balls, coated copper alloy balls, coated tin alloy balls with silicon resin coating or silicon resin coating)・ Coated lead alloy sphere ・ Coated zinc alloy sphere ・ Coated aluminum alloy sphere 2F: Specific critical substance elevating device (Gravity energy is increased and stored) 2H: Chilled seawater mixer (mixed cold water into seawater and overheated in the process of speeding up natural phenomenon) 2X: Air heat exchanger (the air is compressed with a heat pump at a high temperature, aiming at infinite increase in heat recovery compressed air mass or infinite increase in pressure) 2Y: Compressed air heat exchanger ( 2Z: Specific critical material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3A: Water repellent coating, 3D: Electricity + liquid air cold heat + superheated steam heat supply equipment (cooled heat + heat production with gravity power generation electricity, supply liquid oxygen and liquid nitrogen drive car, ship and airplane, supply with superheated steam, recover methane injected into methane hydrate, etc. 3E: Specific critical substances (specific critical substances that are liquid at room temperature, such as mercury and water) 3E: Specific critical substances (low-melting-point liquids that are stable in liquids up to 500 degrees C) 3F: Oxygen pressure reciprocating engine (liquid oxygen, liquid nitrogen and fuel are used as injection combustion 50-200 MPa combustion gas, and fuel injection multistage combustion is driven during expansion process to drive multistage oxygen pressure reciprocating engine) 3G: Theoretical combustion tooth Engine (liquid oxygen + liquid fuel + water is compressed and heated for injection combustion) 3H: reciprocating piston, 3J: theoretical combustion reciprocating engine (liquid oxygen + liquid fuel + water is compressed and heated for injection combustion) 3K: external gear 3L: Multistage combustion chamber, 3M: Steam pressure reciprocating engine (multistage oxygen pressure reciprocating engine heats multistage steam and water to drive the multistage steam pressure reciprocating engine) 3N: Steam pressure gear engine (multistage oxygen pressure gear engine) 3P: Theoretical expansion engine (Boile's law gas volume is inversely proportional to pressure is the best engine) 3R: Theoretical gas turbine (gas volume is pressure) 3S: Theoretical steam turbine (Theoretical best steam turbine that corresponds inversely to the pressure) 3T: Theoretical gas compressor (The gas volume is 3U: Theoretical turbine, 3V: Pump engine (uses existing pumps in the engine) 3X: Compressor engine (uses existing compressors in the engine) 3Y: Counter-rotating engine (Engine whose gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine (liquid oxygen and liquid nitrogen and fuel injection combustion to form 50 to 200 MPa combustion gas, multistage combustion and heating water and water vapor on the inner and outer periphery 3a: Water repellent plating, 3b: Water repellent coating, 4F: Combustion gas reciprocating engine, 4H: Heat absorption tube (long-lens 2d collects sunlight into heat absorption tube in a straight line) 4J: Battery drive wheel, 4K: Theoretical expansion engine vehicle, 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (high temperature in water vapor) 4Z: Combustion gas gear engine, 4X: Turbine blade cross section (cross-sectional area is increased in surface area) 4a: Liquid fuel pump, 4b: Liquid oxygen pump, 4c : Water pump, 4d: Gear device, 4e: Roller, 4f: Rotation support, 5: Air injection nozzle, 5a: High-pressure high-temperature combustion gas control valve, 5b: Compressed intake air passage, 5d: Combustion flow inner wall, 5e: Super High pressure oxygen, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber, 5D: Exhaust valve, 5E: Supply chamber, 5F: Oxygen heating tube, 5G: Steam heating tube, 5H: Water heating tube, 5K: Liquid oxygen, 5K: liquid oxygen chamber, 5L: liquid nitrogen, 5L: liquid nitrogen chamber, 5M: high pressure high temperature combustion gas, 5M: high pressure high temperature combustion gas chamber, 5N: high pressure high temperature steam chamber, 5N: high pressure high temperature steam, 5P: Steam system Valve, 5Q: water control valve, 5R: superheated steam control valve, 5S: compressed air heating pipe, 5T: liquid oxygen control valve, 6: final compression blade, 6A: superheated steam injection nozzle, 6B: compressed air injection nozzle, 6C : Combustion gas water vapor nozzle, 6E: Specific critical substance injection nozzle, 6F: Water injection nozzle, 6G: Stator blade, 6H: Drain pipe, 6L: Oxygen injection nozzle, 6W: Specific critical substance accelerator (liquid specific critical substance 3E pressure 6X: Fuel injection nozzle, 6X: After burner (combustion with the intake air flow and the fuel injection cold heat 28a combustion flow 6Y and increase in the amount of fuel combustion) 6Y: Combustion gas injection nozzle (cooling 28a combustion flow) 6Z: Steam injection nozzle, 7A: Propeller, 7B: Rotating blade, 7C: Screw, 8c: Turbine blade (inner and outer rotor blade groups, respectively) 8d: Upper expansion blade group, 8e: Lower expansion blade group, 8f: Assembly turbine blade group, 8g: Upper compression Blade group, 8h: Lower compression blade group, 8j: Assembly compression blade group, 8H: Vertical type all blade turbine 8H: All-type blade turbine (selecting cemented carbide alloy, silicon resin coating or fluororesin-coated turbine blade) 8H: All-type blade Moving blade water gravity turbine (existing steam turbine is a stationary blade and the damming output is close to 0, so all moving blades are essential, and the work rate is 1 / 360,000 of platinum sphere, so it is essential to use gravity of specific material. 1 to multi-stage heat pump, such as solar heated air Compressed heat is recovered with a compression heat recovery unit, and divided and stored in heat + cold. Turbine drive + used in various applications. 8H: Vertical-type all blade hydrogravity turbine (Heat drive + Cold drive makes the head drop limited. 8K: Vertical type moving blade water gravity turbine (water gravity turbine in which the rotation direction of the outer shaft device and the inner shaft device is alternated by the horizontal axis 1h) 8L: Vertical type moving blade ratio critical material gravity turbine (Specific gravity material gravity turbine in which the rotation direction of the outer shaft device and the inner shaft device is alternated by the horizontal shaft 1h) 8M: Vertical type moving blade water gravity turbine (machined by providing a cylindrical portion on the outer moving blade group of the inner moving blade group) Easy to assemble, easy to lighten) 8N: Gravity turbine with significant ratio of vertical blades (Easy to assemble, easy to assemble, easy to lighten by installing a cylindrical part on the outer blade group of inner blade group) 9: Wear resistance Annular assembly (including 8c 9A: Cylindrical ring assembly (wear-resistant cylindrical ring assembly with 6 types of moving blade groups, easy structure, few parts and fully automatic machining) 9A: Cylindrical annular assembly (inlet fixed outer blade 60E + outer annular blade 60G + outlet fixed outer blade 60J is fitted to form a cylindrical outer moving blade group 60D, and inlet fixed inner blade 60F + inner side) 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 10: Hull, Fitted annular ring 60H + Outlet fixed inner wing 60K 10A: ship cabin, 10b: cockpit, 10c: control room, 10d: cabin, 10e: cargo compartment, 11D: gas cooling room, 16B: vertical axis, 21: solar heater (intake air passage through heat absorption pipe 4H Also provided in 24: Combustion gas control valve, 24A: Compressed air control valve, 24B: Liquid oxygen control valve, 24C: Liquid nitrogen control valve, 24D: Oxygen control valve, 24E: Nitrogen control valve, 25: Superheated steam control Valve, 25b: fuel control valve, 25c: fuel pipe, 28a: air, 28a: cold heat (compressed air 28a is heated by compressing the air 28a with a heat pump, and the compressed air calorie is heated with 50 heat + liquid oxygen or liquid nitrogen) 28b: Compressed air calorie, 28A: Intake air passage, 28B: Air passage inlet, 38: Rotation guide, 38a: Flight trunk, 38b: Flight wing, 38c: Flight tail, 38d: Vertical wing, 38e: Wing leading edge, 38g: surface wing, 38h: levitation boat, 38B: air suction jet ship (with 79S79T79Y79Z) 38C: water suction jet ship (with 79U79X) 39A : Solar Thermal Gravity Airplane, 39B: Solar Thermal Gravity Rotating Airplane, 39C: Solar Thermal Gravity Helicopter, 39D: Screw Ship, 39G: Solar Thermal Gravity Flight Ship, 39H: Oxygen Combined Screw Ship, 39J: Oxygen Combined Injection Ship, 39K: Oxygen Combined Screw Injection Ship, 39L: Oxygen coalescence jet plane, 39M: Oxygen coalescence propeller plane, 39N: Oxygen coalescence propeller jet plane, 39P: Oxygen coalescence rotorcraft, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheated steam 50: Warmth (compressed air 28a is compressed with a heat pump and divided into 50 warm heat of compressed air heat + compressed air 28a cold storage) 50A: steam, 50a: superheated steam injection pipe, 51: air extractor, 5
1: Confluent extractor (extractor for joining) 51A: Air extraction chamber, 52a: Water, 52a: Deep sea water, 52b: Hot water, 52d: Hot heat (change from 50) 52e: Cold heat (change from 28a) 55B: Transmission, 60A: Inner shaft device (equipment with turbine blades) 60B: Outer shaft device (equipment with turbine blades) 60C: Cylindrical inner blade group (including wear-resistant cylindrical annular assembly fixed blades) 60D: Cylindrical outer rotor blade group (Wear resistant cylindrical annular assembly fixed blade group including fully automatic machining easy assembly) 60E: Entrance fixed outer blade (outer rotor blade group annular assembly fixed) 60F: Inlet fixed inner wing (inlet wing for annular assembly fixing inner blade group) 60G: Outer annular wing (intermediate blade for annular assembly of outer blade group) 60H: Inner annular blade (inner blade group) During annular assembly 60J: Outlet fixed outer wing (exit wing for annular assembly fixing outer rotor blade group) 60K: Outlet fixed inner wing (exit wing for annular assembly fixing inner rotor blade group) 76: Gear device (magnetic friction power transmission device) 77B: Semi-cylindrical outer casing, 77F: Injection section outer casing, 77G: Cylindrical rotating section, 77a: Turbine outer casing, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (magnetic bearing + air) 80A: Joint, 80B: Fastening tool, 80E: Liquid coalescence injection part (High pressure high temperature combustion gas 5M High pressure high temperature steam chamber 5N is received and fuel injected and combusted several times in 5M, 5N inner and inner circumference 80F: Liquid combined injection unit (receives high-pressure high-temperature combustion gas 5M high-pressure high-temperature steam chamber 5N, and injects and burns multiple times to 5M, 5N as the inner periphery) Heat multiple times from the inner and outer periphery 80V: Liquid combined injection unit (receives high pressure high temperature combustion gas 5M high pressure high temperature steam chamber 5N and injects fuel multiple times to 5M multiple times. Combustion and 5N is heated and injected several times from the inner circumference, outer circumference, and inner circumference outer circumference, and fuel injection combustion injection is also carried out at a plurality of locations of the air suction flow, and air suction injection is performed) 80W: Liquid combined injection section (high pressure High temperature combustion gas 5M High pressure high temperature steam chamber 5N is received, fuel injection combustion is performed 5M multiple times, 5N is heated and injected multiple times from the inner periphery, outer periphery, and inner periphery outer periphery, and air is sucked and injected) 80S: Liquid air Suction water jet (High pressure high temperature combustion gas 5M High pressure high temperature steam chamber 5N is received and fuel injected and burned to 5M multiple times, and 5N is heated multiple times from the inner circumference, outer circumference and inner circumference outer circumference, and is injected by air suction. 8) T: Liquid air suction water jet (high pressure high temperature combustion gas 5M receiving high pressure high temperature steam chamber 5N, fuel injection combustion in 5M multiple times, and 5N is heated and injected multiple times from the inner circumference, outer circumference and inner circumference outer circumference, 80U: Liquid water suction water jet (high pressure high temperature combustion gas 5M received high pressure high temperature steam chamber 5N to 5M) 80N: Liquid water suction water jet (high-pressure high-temperature combustion gas 5M high-pressure high-temperature steam chamber 5N) 80N: Liquid air suction water jet (high pressure and high temperature combustion) 80Y: Liquid air suction water jet (high pressure high temperature combustion) 80Z: receiving 5S high-pressure high-temperature steam chamber 5N, fuel-injecting and burning multiple times to 5M, heating and injecting 5N multiple times from the inner periphery and inner periphery, and sucking and injecting water by air suction) Liquid air suction water jet (High pressure high temperature combustion gas 5M High pressure high temperature steam chamber 5N is received and fuel injected and burned into 5M multiple times, and 5N is heated and injected multiple times from the inner circumference and inner circumference outer circumference, multiple air suction flows 84: Counter-rotating magnetic friction device (with fixed portion, rotating inner blade group and outer blade group at substantially the same speed and opposite rotation) 84Y: Counter-rotating gear device (device that counter-rotates with existing technology) 85: Counter-rotating magnetic device (magnet-use gear height is slight to non-contact, and the shaft 1h gear is used to rotate counterclockwise) 85Y : Counter rotating gear device (existing horizontal shaft 1h 88A: Oxygen coalesced air injection unit (rocket combustion + jet combustion + steam injection, etc.) 88K: Oxygen coalescence water injection unit (rocket combustion + jet combustion + steam injection, etc.) 95a: combustion gas reservoir, 95b: compressed air reservoir, 95c: superheated steam reservoir, 103: cold heat recovery device,

Claims (371)

夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type blades each with wear-resistant super water-repellent plating (3a), a cylindrical annular assembly (9A), and a magnetically utilized bearing load close to a vertical type all-blade specific material gravity turbine (8N) 1 ~ 20 energy storage cycle coalescence engine and coalescence method for generating 20 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each type of blade-type all-blade specific gravity turbine (8N) 21 with a magnetic bearing load approaching zero with six types of blade groups, each with a wear-resistant super-water-repellent plating (3a) and a cylindrical annular assembly (9A). Various energy storage cycle coalescence engine and coalescence method for generating 40 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each type of blade-type all-blade specific gravity turbine (8N) 41 with a magnetic bearing load approaching zero with six types of blade groups, each with a wear-resistant super water-repellent plating (3a), and a cylindrical annular assembly (9A). Various energy storage cycle coalescence engines and coalescence methods for generating -60 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type blades each with wear-resistant super-water-repellent plating (3a), a cylindrical annular assembly (9A), and a magnetically-enhanced bearing blade load critical approach gravity turbine (8N) 61 ˜80 sets of various energy storage cycle coalescing engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type of blade group each made of wear-resistant super water-repellent plating (3a), a cylindrical annular assembly (9A) and a magnetically utilized bearing load close to a vertical all-blade ratio critical material gravity turbine (8N) 81 ˜100 sets of various energy storage cycle coalescence engines and coalescence methods. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type blades each with wear-resistant super water-repellent plating (3a), a cylindrical annular assembly (9A), and a magnetically utilized bearing load close to a vertical type full blade ratio material gravity turbine (8N) 101 Various energy storage cycle coalescence engines and coalescence methods for generating 120 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type of blade group each made of wear-resistant super water-repellent plating (3a), a cylindrical annular assembly (9A) and a magnetically utilized bearing load close to a vertical type all-blade specific material gravity turbine (8N) 121 Various energy storage cycle coalescence engine and coalescence method for generating 140 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each type of blade-type all-blade specific gravity gravity turbine (8N) 141 with a magnetic bearing load approaching zero with six types of blade groups each made of a wear-resistant super-water-repellent plating (3a) and a cylindrical annular assembly (9A). Various energy storage cycle coalescence engines and coalescence methods for generating 160 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each type of blade-type all-blade specific gravity gravity turbine (8N) 161 with a magnetic bearing load approaching zero with six types of blade groups each made of a wear-resistant super-water-repellent plating (3a) and a cylindrical annular assembly (9A) Various energy storage cycle coalescence engines and coalescence methods for generating 180 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 type blades each with wear-resistant super-water-repellent plating (3a), a cylindrical annular assembly (9A), and a magnetically utilized bearing load close to a vertical type all-blade specific material gravity turbine (8N) 181 Various energy storage cycle coalescence engine and coalescence method for generating 200 sets of power. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of vertical turbine moving blade ratio critical material gravity turbine (8N). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating 21 to 40 sets of vertical turbine gravity blade (8N) serious material gravity turbine (8N). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of gravity turbine (8N) vertical material gravity turbine significant material gravity turbine. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various energy storage cycle coalescence engine and coalescence method for generating a power generator of a vertical all-blade ratio critical material gravity turbine (8N) 61-80. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various energy storage cycle coalescence engine and coalescence method for generating a power generator of a vertical all-blade ratio critical material gravity turbine (8N) 81-100. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating a power generator of a vertical all blade ratio critical material gravity turbine (8N) 101-120. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating a power generation of a vertical all-blade ratio critical material gravity turbine (8N) 121-140. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating a power generator with a vertical all blade ratio critical material gravity turbine (8N) 141-160. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Each of the six types of rotor blades is a cylindrical annular assembly (9A), which is a wear-resistant super-water-repellent plating (3a), and a magnetic material bearing load that is driven by injection with Mach 1 to 3 is used. Various types of energy storage cycle coalescence engine and coalescence method for generating a power generator with a vertical all-blade ratio critical material gravity turbine (8N) 161-180. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆入口固定外翼(60E)+外側環状翼(60G)+出口固定外翼(60J)嵌合で円筒外側動動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 types of moving blade groups each made of wear-resistant super-water-repellent plating (3a), cylindrical material (9A) and specific material (3E) Mach 1 to 3 fixed injection blades (60E) + outer Various types of power generation for vertical turbine blades (8N) 181 to 200 sets, which are close to the vertical type rotor blades with a magnetic bearing load of 0, which moves to the outside of the cylinder by fitting an annular blade (60G) + outlet fixed outer blade (60J). Energy conservation cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load of 0 approach to drive. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engines and coalescence methods for generating 21 to 40 sets of saddle type all-blade ratio critical material gravity turbine (8N) with a magnetic bearing load of 0 approach to drive. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engines and coalescence methods for generating 41-60 sets of vertical turbine blades critical material gravity turbine (8N) with a magnetic load bearing approaching zero driving. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engines and coalescence methods for generating 61 to 80 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load to be driven approaching zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engine and coalescence method for generating a power generation using a magnetically driven bearing with a magnetic bearing ratio of 0 to 100 sets of gravity type gravity turbine (8N). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engine and coalescence method for generating a power generation by using a magnetically-driven bearing with a magnetic bearing ratio of 0 approaching to a vertical all-blade ratio critical material gravity turbine (8N) 101-120 power generation. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescing engine and coalescence method for generating a power generation using a magnetically driven bearing with a driving force close to a vertical all blade ratio material gravity turbine (8N) 121-140 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engine and coalescence method for generating a power generation by using a magnetically-driven bearing having a magnetic load of nearly 0 and a set of all-blade blade ratio critical material gravity turbine (8N) 141-160 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescing engine and coalescence method for generating a power generation by using a magnetically driven bearing having a magnetic load of nearly 0 and a set of all-blade blade critical material gravity turbines (8N) 161-180. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various energy storage cycle coalescence engines and coalescence methods for generating a power generation by using a magnetically-driven bearing with a magnetic bearing ratio of 0 approaching to a power generator of a vertical type all-blade ratio gravity gravity (8N) 181 to 200 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) set to 0 approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a power generation of 21 to 40 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) that is close to zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating 41 to 60 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) set to 0 approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating power of 61 to 80 sets of saddle-type all-blade ratio critical material gravity turbine (8N) set to 0 approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating a power generation of 81 to 100 sets of saddle-type all-blade ratio critical material gravity turbine (8N) that is close to zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating a power generator with a total gravity ratio of 8 to 100, which is close to zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a power generator with a total gravity ratio of 8 to 121, which is close to zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating a power generator with a total gravity ratio of 8 (N) 141-160, which is close to zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating a power generator with a total gravity of (8N) 161 to 180 in a vertical all-blade ratio critical material with zero approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetic bearing load that is driven by counter rotation or generator (1) by horizontal axis (1h) with 6 types of moving blades grouped as cylindrical annular assembly (9A), each of which is wear resistant super water-repellent plating (3a). Various energy storage cycle coalescing engine and coalescence method for generating a power generator with a total gravity ratio of 8 to 187-200. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of vertical type moving blade ratio critical material gravity turbine (8N) driven by reversal drive and generator (1) driven magnetic bearing load approaching 0. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engines and coalescence methods for generating 21 to 40 sets of vertical turbine moving blade ratio critical material gravity turbines (8N) driven by reversal drive and generator (1) driven magnetic bearing load close to 0. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) driven by reversal drive and generator (1) driven magnetically utilized bearing load approaching zero. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engine and coalescence method for generating 61-80 sets of saddle type full blade ratio material gravity turbine (8N) driven by reversal drive and generator (1) driven magnetic load. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation by using a vertical type moving blade ratio critical material gravity turbine (8N) 81 to 100 in which the load is close to 0 using a magnetic bearing for reversal drive and generator (1) drive. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8N) 101-120 that is driven by reversal drive and generator (1) and uses a magnetic bearing load close to 0. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8N) 121-140 in which reversal drive and generator (1) drive are used in a magnetic bearing load of 0 approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescing engines and coalescence methods for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8N) 141-160 in which the load is close to zero using a magnetic bearing for driving inversion and generator (1). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engine and coalescence method for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8N) 161-180 that is driven by reversal drive or generator (1) and uses magnetic bearing load close to 0. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   A horizontal axis (1h) driven by injection with specific material (3E) Mach 1 to 3 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Various energy storage cycle coalescence engine and coalescence method for generating 181 to 200 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) 181-200 sets with a magnetically utilized bearing load approaching 0 for reversal drive and generator (1) drive. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 sets of vertical type moving blade ratio critical material gravity turbine (8N) driven near to zero using a magnetic bearing load to drive and generator (1). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engines and coalescence methods for generating power to generators (1) 21 to 40 sets of vertical turbine blade ratio critical material gravity turbines (8N) driven by a magnetically utilized bearing load to drive (1). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) driven near the driving load and generator (1) using a magnetic bearing. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engines and coalescence methods for generating 61-80 sets of saddle-type all-blade ratio critical material gravity turbine (8N) driven near the drive and generator (1) driving magnetic bearing load 0 approach. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engines and coalescence methods for generating 81 to 100 sets of vertical-type full blade ratio material gravity turbine (8N) driven with a magnetic bearing load of 0 driving and generator (1) approaching. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engine and coalescence method for generating a power generation by using a magnetically driven bearing with a magnetic bearing (0) approaching to a generator and a generator (1). 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engine and coalescence method for generating power to generator / generator (1) driven by magnetically utilized bearing load of 0-type full blade ratio critical material gravity turbine (8N) 121-140 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engines and coalescence methods for generating power to generators and generators (1) driven by magnetically utilized bearings with a load of 0-type full blade ratio critical material gravity turbine (8N) 141-160 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engine and coalescence method for generating power to generator / generator (1) driven by magnetically utilized bearing load near zero vertical blade ratio critical material gravity turbine (8N) 161-180 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 anti-water repellent plating (3a), 6 types of moving blade groups (9A), cylindrical material (9A), specific material (3E) Mach 1 or more, the horizontal axis (1h) driven by injection is double reversed Various energy storage cycle coalescence engine and coalescence method for generating power to generator and generator (1) driven by a magnetically utilized bearing load of 0-type full blade ratio critical material gravity turbine (8N) 181 to 200 sets. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various energy storage to generate 1-20 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with close to zero bearing load approaching zero with counter rotation drive and generator (1) driven on horizontal axis (1h) Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy storage to generate power from 21 to 40 sets of vertical-type full-blade specific material gravity turbine (8N) driven with double reversal drive on the horizontal axis (1h) and generator (1) driven with magnetic bearing load approaching 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate 41-60 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with double reversal drive on the horizontal axis (1h) and generator bearing (1) driven with a magnetic bearing load approaching 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate power from 61 to 80 sets of vertical full-blade specific material gravity turbine (8N) driven by double reversal drive on the horizontal axis (1h) and generator (1) driven with a magnetic bearing load approaching 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate power in a vertical type moving blade ratio critical material gravity turbine (8N) 81 to 100 sets with a double reversal drive on the horizontal axis (1h) or a generator bearing (1) driven by a magnetic bearing load close to 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate power in a vertical type moving blade ratio critical material gravity turbine (8N) 101-120 set with a magnetic reversal bearing load approaching zero with a counter-rotating drive or generator (1) driven on the horizontal axis (1h) Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy storage to make power generation of vertical turbine blades (8N) 121-140 sets, which are driven by double reversal drive on the horizontal axis (1h) and generator bearings (1) and with a magnetic bearing load of 0 approach. Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate power in a vertical type moving blade ratio critical material gravity turbine (8N) 141-160 set with a double reversal drive on the horizontal axis (1h) and a generator bearing (1) driven by a magnetic bearing load close to 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy conservation to generate power in the vertical type moving blade ratio critical material gravity turbine (8N) 161-180 set with a double reversal drive on the horizontal axis (1h) and a generator bearing (1) driven by a magnetic bearing load close to 0 Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1以上で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Highly water-resistant repellent plating (3a), 6 types of blades with cylindrical ring assembly (9A), specific material (3E) Mach 1 or more, and injection ratio material (2E) is mixed and accelerated. Various types of energy storage to generate a power generator of a vertical type moving blade ratio critical material gravity turbine (8N) 181 to 200 sets in which the horizontal shaft (1h) is driven in a counter-rotating manner and the generator (1) is driven by a magnetic bearing. Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜20組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   6 types of moving blade groups each made of wear-resistant super-water-repellent plating (3a) and cylindrical ring assembly (9A) specific material (3E) Mach 1 to 3 injection ratio critical material (2E) mixed injection acceleration drive Various energy storage to generate 1-20 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with close to zero bearing load approaching zero with counter rotation drive and generator (1) driven on horizontal axis (1h) Cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)21〜40組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power from 21 to 40 sets of vertical full blade ratio material gravity turbine (8N) driven with counter rotating drive on the horizontal axis (1h) to drive or generator bearing (1) with magnetic utilization bearing load approaching 0 Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)41〜60組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate 41-60 sets of vertical full-blade ratio critical material gravity turbine (8N) in which the horizontal axis (1h) to be driven is double reversal drive and the generator (1) is driven by magnetism and the bearing load is close to 0 Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)61〜80組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate 61-80 sets of vertical all-blade ratio critical material gravity turbine (8N) in which the horizontal axis (1h) to be driven is double reversal drive and the generator (1) is driven by magnetism and the bearing load is close to 0 Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)81〜100組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a vertical type moving blade ratio critical material gravity turbine (8N) 81-100 with double reversal drive on the driven horizontal axis (1h) and generator bearings (1) with a magnetic bearing load approaching 0 Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)101〜120組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a pair of vertical all-blade ratio critical material gravity turbine (8N) 101-120 with a double reversal drive on the driven horizontal axis (1h) and a magnetic bearing load approaching 0 for driving the generator (1) Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)121〜140組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a vertical all-blade ratio critical material gravity turbine (8N) 121-140 set with a double reversal drive on the driven horizontal axis (1h) and a magnetic bearing load approaching 0 on the generator (1) drive Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)141〜160組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a vertical all-blade ratio critical material gravity turbine (8N) 141-160 with a counter rotating drive on the horizontal axis (1h) to be driven and a magnet bearing load approaching 0 to drive a generator (1) Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)161〜180組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a vertical all-blade ratio critical material gravity turbine (8N) 161-180 set with a double reversal drive on the driving horizontal axis (1h) and a magnetic bearing load approaching 0 for driving the generator (1) Storage cycle coalescence engine and coalescence method. 夫々耐摩耗超撥水鍍金(3a)とした、6種類の動翼群を円筒環状組立(9A)とした比重大物質(3E)マッハ1〜3で噴射比重大物質(2E)を混合噴射加速駆動する横軸(1h)で二重反転駆動や発電機(1)駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)181〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Accelerated mixing injection of critical material (2E) with specific critical material (3E) Mach 1 to 3 with 6 types of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Various types of energy to generate power in a vertical type moving blade ratio critical material gravity turbine (8N) 181 to 200 sets in which the horizontal axis (1h) to be driven is a counter-rotating drive and the generator (1) is driven to use a magnetic bearing. Storage cycle coalescence engine and coalescence method. 外側軸装置(60B)と円筒環状組立(9A)を入口固定外翼(60E)環状嵌合組立固定で耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)の入口動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Inlet blade of the cylindrical outer blade group (60D) in which the outer shaft device (60B) and the cylindrical annular assembly (9A) are wear-resistant superhydrophobic plating (3a) by fixing the inlet fixed outer blade (60E) annular fitting assembly. Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of saddle type all-blade ratio critical material gravity turbines (8N) having a bearing load approaching zero constituting the group. 内側軸装置(60A)と円筒環状組立(9A)を入口固定内翼(60F)環状嵌合組立固定で耐摩耗超撥水鍍金(3a)とした円筒内側動翼群(60C)の入口動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Inlet blade of the cylindrical inner blade group (60C) in which the inner shaft device (60A) and the cylindrical annular assembly (9A) are wear-resistant super water-repellent plating (3a) by fixing the inlet fixed inner blade (60F) annular fitting assembly. Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of saddle type all-blade ratio critical material gravity turbines (8N) having a bearing load approaching zero constituting the group. 外側軸装置(60B)と円筒環状組立(9A)を外側環状翼(60G)環状嵌合組立で耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)の外側中間動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   The outer intermediate blade group of the cylindrical outer blade group (60D) in which the outer shaft device (60B) and the cylindrical annular assembly (9A) are made of an outer annular blade (60G) annular fitting assembly and wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating 1 to 200 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero. 内側軸装置(60A)と円筒環状組立(9A)を内側環状翼(60H)環状嵌合組立で耐摩耗超撥水鍍金(3a)とした円筒内側動翼群(60C)の内側中間動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Inner intermediate blade group of cylindrical inner blade group (60C) in which inner shaft device (60A) and cylindrical annular assembly (9A) are wear-resistant super-water-repellent plating (3a) by inner annular blade (60H) annular fitting assembly. Various energy storage cycle coalescence engine and coalescence method for generating 1 to 200 sets of vertical turbine moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero. 外側軸装置(60B)と円筒環状組立(9A)を外側環状翼(60G)環状嵌合組立で耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)の外側中間動翼群を2回以上構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   The outer intermediate blade group of the cylindrical outer blade group (60D) in which the outer shaft device (60B) and the cylindrical annular assembly (9A) are made of an outer annular blade (60G) annular fitting assembly and wear-resistant super-water-repellent plating (3a). 2 types of energy storage cycle coalescence engine and coalescence method for generating 1 to 200 sets of gravity-type all-blade ratio critical material gravity turbine (8N) having a magnetic bearing load approaching zero. 内側軸装置(60A)と円筒環状組立(9A)を内側環状翼(60H)環状嵌合組立で耐摩耗超撥水鍍金(3a)とした円筒内側動翼群(60C)の内側中間動翼群を2回以上構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Inner intermediate blade group of cylindrical inner blade group (60C) in which inner shaft device (60A) and cylindrical annular assembly (9A) are wear-resistant super-water-repellent plating (3a) by inner annular blade (60H) annular fitting assembly. 2 types of energy storage cycle coalescence engine and coalescence method for generating 1 to 200 sets of gravity-type all-blade ratio critical material gravity turbine (8N) having a magnetic bearing load approaching zero. 内側軸装置(60A)と円筒環状組立(9A)を出口固定内翼(60K)環状嵌合組立固定で耐摩耗超撥水鍍金(3a)とした円筒内側動翼群(60C)の出口動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Outlet blades of the cylindrical inner blade group (60C) in which the inner shaft device (60A) and the cylindrical annular assembly (9A) are made of an abrasion-fixed superhydrophobic plating (3a) by fixing the outlet fixed inner blade (60K) annular fitting assembly. Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of saddle type all-blade ratio critical material gravity turbines (8N) having a bearing load approaching zero constituting the group. 外側軸装置(60B)と円筒環状組立(9A)を出口固定外翼(60J)環状嵌合組立固定で耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)の出口動翼群を構成する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   Outlet blades of the cylindrical outer blade group (60D) in which the outer shaft device (60B) and the cylindrical annular assembly (9A) are wear-resistant super water-repellent plating (3a) by fixing the outlet fixed outer blade (60J) to the annular fitting assembly. Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of saddle type all-blade ratio critical material gravity turbines (8N) having a bearing load approaching zero constituting the group. 外側軸装置(60B)+耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)を横軸(1h)歯車で連結駆動することで次の外側軸装置(60B)+円筒外側動翼群(60D)回転方向を逆回転として共振や騒音を僅少にする磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   The next outer shaft device (60B) + the outer side of the cylinder is driven by connecting the outer shaft device (60B) + the cylindrical outer blade group (60D) made of the wear-resistant super-water-repellent plating (3a) with a horizontal shaft (1h) gear. Various types of energy storage to generate power generation of gravity turbine (8N) 1 ~ 200 sets of vertical type blades with a magnetic bearing load close to 0 using magnetic force to reduce resonance and noise by rotating the blade group (60D) in the reverse direction. Cycle coalescence engine and coalescence method. 外側軸装置(60B)+耐摩耗超撥水鍍金(3a)とした円筒外側動翼群(60D)を横軸(1h)歯車で連結駆動することで次の外側軸装置(60B)+円筒外側動翼群(60D)回転方向を逆回転として共振や騒音を僅少にして内側軸装置(60A)と二重反転駆動する磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)1〜200組発電にする各種エネルギ保存サイクル合体機関及び合体方法。   The next outer shaft device (60B) + the outer side of the cylinder is driven by connecting the outer shaft device (60B) + the cylindrical outer blade group (60D) made of the wear-resistant super-water-repellent plating (3a) with a horizontal shaft (1h) gear. Rotor blade group (60D) vertical-type full blade ratio material gravity turbine (60m) with a reverse rotation and a low resonance and noise to make it close to the inner shaft device (60A) and a magnetically utilized bearing load that double-reversely drives. 8N) Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of power. 太陽光加熱器(21)を水面に浮力を設けて具備して、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   A solar-powered heater (21) is provided with buoyancy on the water surface, and solar-heated air is a vertical all-blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero. 1 to the multistage heat pump (1G), and the intake is compressed several times, and heat is recovered by the 1 to multistage compression heat recovery unit (2C) for each compression, and electricity + liquid air cold heat + superheated steam temperature supply equipment ( 3D) Various energy storage cycle coalescence engines and coalescence methods. 太陽光加熱器(21)を水面に浮力を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   A solar heater (21) is provided with buoyancy on the water surface, and a rotation support part (4f) for controlling rotation of the sunlight at right angles from east to west is provided, and the solar heating air is used as a magnetic bearing load. Zero-type all-blade ratio critical material gravity turbine (8N), which is close to 0, is compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, and 1 to multi-stage compression heat for each compression Various energy storage cycle coalescence engines and coalescence methods for recovering heat with a recovery device (2C) to make electricity + liquid air cold heat + superheated steam temperature supply equipment (3D). 太陽光加熱器(21)を水面に浮力を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) Is a cylindrical rotating part (77G), which is a device that controls the rotation of sunlight at a right angle in the vertical direction, and a vertical all-blade ratio critical material gravity turbine (8N) with solar heated air approaching a magnetic bearing load of 0 Low power generation electric drive, 1 to multi-stage heat pump (1G) compresses several times with suction, 1 to multi-stage compression heat recovery device (2C) recovers heat for each compression, electricity + liquid air cold heat + superheat Various energy storage cycle coalescence engines and coalescence methods for steam temperature and heat supply equipment (3D). 太陽光加熱器(21)を水面に浮力を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、浮力利用により東西方向直角維持回転制御する装置として、太陽光を熱吸収管(4H)中心に直線照射内部空気(28a)温度を最高にし、磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), as a device for controlling rotation of the sunlight at a right angle in the vertical direction and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy, the sunlight is linearly irradiated around the center of the heat absorption tube (4H). Vertically moving blade ratio critical material gravity turbine (8N) with maximum air (28a) temperature and close to magnetic utilization bearing load of 0 Various energy storage cycle coalescence engines and coalescence methods that are recompressed and heat-recovered with a 1 to multiple-stage compression heat recovery device (2C) for each compression to make electricity + liquid air cold heat + superheated steam temperature supply equipment (3D). 太陽光加熱器(21)を水面に浮力を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、浮力利用により東西方向直角維持回転制御する装置として、太陽光を熱吸収管(4H)中心に直線照射内部空気(28a)温度を最高にし、外部空気(28a)も加熱夫々の空気路(28A)高温度選択吸入として、磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), as a device for controlling rotation of the sunlight at a right angle in the vertical direction and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy, the sunlight is linearly irradiated around the center of the heat absorption tube (4H). A vertical type full-blade ratio critical material gravity turbine (8N) in which the temperature of the air (28a) is maximized and the external air (28a) is also heated for each air passage (28A) as a high-temperature selective suction, and the bearing load is close to zero using magnetism. Compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, heat is recovered with 1 to multi-stage compression heat recovery unit (2C) for each compression, and electricity + liquid air cooling + Superheated steam temperature supply equipment (3D) Various energy conservation cycle combined institutions and coalescence how to. 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   A solar-powered heater (21) equipped with a circular railroad on a flat ground, and a vertical-type all-blade blade critical material gravity turbine (8N) with solar-heated air approaching a magnetic bearing load of 0 Drive, compress multiple times with 1 to multi-stage heat pump (1G), recover heat with 1 to multi-stage compression heat recovery unit (2C) for each compression, electricity + liquid air cold heat + superheated steam temperature supply equipment (3D) Various energy storage cycle coalescence engines and coalescence methods. 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling and rotating the sunlight at a right angle from east to west, and the solar heating air is used as a magnetic bearing. A vertical all-blade ratio critical material gravity turbine (8N) with a load approaching zero (8N) is a very inexpensive power generation electric drive, 1 to multi-stage heat pump (1G), compressed multiple times by suction, 1 to multi-stage compression for each compression Various energy storage cycle coalescence engines and coalescence methods that recover heat with a heat recovery device (2C) to make electricity + liquid air cold heat + superheated steam temperature heat supply equipment (3D). 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、太陽光加熱空気を磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling rotation of the sunlight at a right angle from east to west, and a gear device (4d) and a roller ( 4e) As a cylindrical rotating part (77G), a vertical rotating blade maintaining device is controlled so that sunlight is maintained at a right angle in the vertical direction. Compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, heat is recovered with 1 to multi-stage compression heat recovery unit (2C) for each compression, and electricity + liquid air cooling + Various energy storage cycle coalescence engines and coalescence methods for superheated steam temperature supply equipment (3D). 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、円形鉄道利用により東西方向直角維持回転制御する装置として、太陽光を熱吸収管(4H)中心に直線照射内部空気(28a)温度を最高にし、磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling rotation of the sunlight at a right angle from east to west, and a gear device (4d) and a roller ( 4e) is used as a cylindrical rotating part (77G) as a device for controlling and rotating sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east and west direction by using a circular railway, sunlight is linearly centered on the heat absorption tube (4H). A vertical multi-blade ratio critical material gravity turbine (8N) with the highest irradiation internal air (28a) temperature and close to the magnetic bearing load of 0 Various energy storage cycle coalescence engines and coalescences that are compressed multiple times by suction and heat is recovered by 1 to multi-stage compression heat recovery unit (2C) for each compression to make electricity + liquid air cold heat + superheated steam temperature supply facility (3D) Method. 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光を東から西に直角維持回転制御する回転支持部(4f)等を具備し、歯車装置(4d)やローラー(4e)により円筒回転部(77G)として、太陽光を上下方向直角維持回転制御する装置とし、円形鉄道利用により東西方向直角維持回転制御する装置として、太陽光を熱吸収管(4H)中心に直線照射内部空気(28a)温度を最高にし、外部空気(28a)も加熱夫々の空気路(28A)高温度選択吸入として、磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、1〜複数段熱ポンプ(1G)で吸入複数回圧縮し、圧縮毎に1〜複数段圧縮熱回収器(2C)で熱回収して、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)にする各種エネルギ保存サイクル合体機関及び合体方法。   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling rotation of the sunlight at a right angle from east to west, and a gear device (4d) and a roller ( 4e) is used as a cylindrical rotating part (77G) as a device for controlling and rotating sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east and west direction by using a circular railway, sunlight is linearly centered on the heat absorption tube (4H). A vertical full blade ratio material gravity turbine (maximizing the inner bearing (28a) temperature and the external air (28a) is also heated for each air passage (28A) as a high-temperature selective intake, with a magnetic bearing load approaching zero ( 8N) Extremely inexpensive electricity-driven electric drive, 1 to multi-stage heat pump (1G) compressed by suction multiple times, and heat is recovered by 1 to multi-stage compression heat recovery unit (2C) for each compression, electricity + liquid air Cold heat + superheated steam temperature supply equipment Various energy conservation cycle combined institutions and coalescence how to 3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、海底のメタンハイドレートに過熱蒸気温熱注入メタンを回収する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Received from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low cost electricity production, Various energy storage cycle coalescing engine and coalescence method for recovering methane hydrate with superheated steam hot injection methane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、海底のメタンハイドレートに過熱蒸気温熱注入メタンを液体窒素(5L)冷却液体メタンで回収する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Received from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low cost electricity production, Various energy storage cycle coalescence engines and coalescence methods for recovering methane hydrate with superheated steam hot-injected methane with liquid nitrogen (5 L) cooled liquid methane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、永久凍土地下のメタンハイドレートに過熱蒸気温熱注入メタンを回収する各種エネルギ保存サイクル合体機関及び合体方法。   Perpendicular frozen soil received from an electricity + liquid air cold heat + superheated steam heat supply facility (3D) of extremely low-cost power generation electricity production Various energy conservation cycle coalescence engines and coalescence methods for recovering superheated steam hot methane injection into underground methane hydrate. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、永久凍土地下のメタンハイドレートに過熱蒸気温熱注入メタンを液体窒素(5L)冷却液体メタンで回収する各種エネルギ保存サイクル合体機関及び合体方法。   Perpendicular frozen soil received from an electricity + liquid air cold heat + superheated steam heat supply facility (3D) of extremely low-cost power generation electricity production Various energy storage cycle coalescence engines and coalescence methods for recovering superheated steam hot methane injection into underground methane hydrate with liquid nitrogen (5 L) cooled liquid methane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、永久凍土地下のメタンハイドレートに過熱蒸気温熱注入囲い設けてメタン回収や牧草地放牧事業等にする各種エネルギ保存サイクル合体機関及び合体方法。   Perpendicular frozen soil received from an electricity + liquid air cold heat + superheated steam heat supply facility (3D) of extremely low-cost power generation electricity production Various energy conservation cycle coalescence engine and coalescence method for methane recovery and pasture grazing business by installing superheated steam heat injection enclosure in underground methane hydrate. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、オイルサンド地帯に過熱蒸気注入囲い設けて回収する各種エネルギ保存サイクル合体機関及び合体方法。   An all-blade type blade with a magnetic bearing load approaching zero Gravity turbine (8N) Received from the electricity + liquid air cold heat + superheated steam temperature heat supply equipment (3D) of extremely low cost electricity production, oil sand Various energy storage cycle coalescence engines and coalescence methods for recovering by providing superheated steam injection enclosure in the zone. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、オイルシェール地帯に過熱蒸気注入囲い設けて回収する各種エネルギ保存サイクル合体機関及び合体方法。   An oil shale is received from an electricity + liquid air cold heat + superheated steam temperature supply facility (3D), which is an extremely inexpensive generator for electric power production, with a vertical type moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching 0 Various energy storage cycle coalescence engines and coalescence methods for recovering by providing superheated steam injection enclosure in the zone. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、老朽石油採取地帯に過熱蒸気注入囲い設けて回収する各種エネルギ保存サイクル合体機関及び合体方法。   A type of all-wheel blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Received from electricity + liquid air cold heat + superheated steam temperature supply facility (3D) of extremely low-priced power generation electricity production, old oil Various energy storage cycle coalescence engines and coalescence methods for collecting and collecting superheated steam injection enclosures in the sampling zone. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より受給して、食品製造業等では過熱蒸気安価受給して安価食料品大量生産にする各種エネルギ保存サイクル合体機関及び合体方法。   Magnetically used bearing load approaching zero vertical type rotor blade critical material gravity turbine (8N) Extremely inexpensive power generation electricity production, electricity + liquid air cold heat + superheated steam temperature supply facility (3D), food production Various energy conservation cycle coalescence engines and coalescence methods for receiving low-cost superheated steam and mass production of cheap food products in the industry. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価過熱蒸気を受給して、農業用や工業用や産業用や鉱業用に使用して温熱利用全盛にする各種エネルギ保存サイクル合体機関及び合体方法。   Low-power superheated steam is received from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely low-cost power generation electricity production of vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 Various energy conservation cycle coalescence engines and coalescence methods used for agriculture, industrial, industrial and mining industries to make the best use of heat. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して自動車駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that aims to increase combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) As a super-high pressure fuel combustion, the theoretical expansion engine (3P) is driven to drive the automobile and various energy storage cycle combined engines And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して自動車駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Various energy storage cycle coalescence engines and coalescence methods that drive a theoretical expansion engine (3P) as an ultrahigh pressure fuel combustion and drive an automobile. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して自動車駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production A theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims at increased combustion of oxygen and hydrogen. (4Y) Various energy storage cycle coalescence engines and coalescence methods that drive a theoretical expansion engine (3P) as an ultra-high pressure fuel combustion and drive an automobile. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression (4Y) to the theoretical expansion engine (3P) driven generator (1) driven storage battery (1A) as ultra high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods for storing and driving storage battery drive wheels (4J) rotation theoretical expansion engine automobiles (4K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims to increase combustion with oxygen and hydrogen (4Y) Superhigh pressure fuel combustion Theoretical expansion engine (3P) Drive generator (1) Drive storage battery (1A) Various energy storage cycle coalescence engine and coalescence method for driving a rotational expansion engine automobile (4K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen (4Y), theoretical expansion engine (3P) drive generator (1) drive storage battery (1A) and storage battery drive wheel (4J) Rotation Theory Expansion Engine Vehicle (4K) Various energy storage cycle merging engines and merging methods for driving. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転と普通車輪回転が可能な理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression (4Y) to the theoretical expansion engine (3P) driven generator (1) driven storage battery (1A) as ultra high pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a theoretical expansion engine automobile (4K) capable of storing and rotating a storage battery drive wheel (4J) and a normal wheel. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転と普通車輪回転が可能な理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims to increase combustion with oxygen and hydrogen (4Y) Superhigh pressure fuel combustion Theoretical expansion engine (3P) Drive generator (1) Drive storage battery (1A) Various energy storage cycle coalescence engine and coalescence method driven by a theoretical expansion engine automobile (4K) capable of rotating and rotating normal wheels. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動発電機(1)駆動蓄電池(1A)に蓄電して蓄電池駆動車輪(4J)回転と普通車輪回転が可能な理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen (4Y), theoretical expansion engine (3P) drive generator (1) drive storage battery (1A) and storage battery drive wheel (4J) Various energy storage cycle coalescence engines and coalescence methods driven by a theoretical expansion engine automobile (4K) capable of rotating and rotating normal wheels. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して理論膨張機関自動車(4K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression and driving the theoretical expansion engine (3P) and driving the theoretical expansion engine automobile (4K) as ultra-high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression (4Y) Various types of driving the theoretical expansion engine (3P) and the screw (7C) rotating ship as super high pressure fuel combustion Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Various energy storage cycle coalescence engines and coalescence methods that drive the theoretical expansion engine (3P) and drive the screw (7C) as a high pressure fuel combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam receiving theoretical combustion chamber (4Y) aiming for increased combustion of oxygen and hydrogen (4Y) Driven by a theoretical expansion engine (3P) as an ultra-high pressure fuel combustion and various energy storage cycle coalescing engines driven by a screw (7C) rotating ship and Merge method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) Super-high pressure fuel combustion 1 to multiple drives of the theoretical expansion engine (3P) and multiple rotations of the screw (7C) Various energy storage cycle coalescence engines and coalescence methods for driving a ship. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at oxygen-oxygen-enhanced combustion Combustion engine (4Y) Ultra-high-pressure fuel combustion Various energy storage cycle coalescence engines that drive 1 to 2 and drive multiple screws (7C) And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Receiving superheated steam, theoretical combustion chamber (4Y) aiming for increased combustion of oxygen and hydrogen (4Y) Super-high pressure fuel combustion Theoretical expansion engine (3P) 1 to multiple drive and screw (7C) multiple rotation ship drive to save various energy Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体スクリュー船舶(39H)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) Super-high pressure fuel combustion 1 to multiple drives of the theoretical expansion engine (3P) and multiple rotations of the screw (7C) Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence screw ship (39H). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体スクリュー船舶(39H)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Drives the theoretical expansion engine (3P) 1 to multiple drives to drive the screw (7C) multi-turn oxygen combined screw ship (39H) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体スクリュー船舶(39H)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives overheated steam and aims to increase combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drives as a high-pressure fuel combustion screw (7C) multi-rotation oxygen combined screw ship (39H ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して酸素合体スクリュー船舶(39H)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression and driving the theoretical expansion engine (3P) as an ultra-high pressure fuel combustion and driving the oxygen combined screw ship (39H) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression and driving the theoretical expansion engine (3P) as super high pressure fuel combustion and screw (7C) rotary oxygen combined water injection (88K) injection propulsion ship various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Drives the theoretical expansion engine (3P) as an ultra-high pressure fuel combustion and drives the screw (7C) rotary oxygen combined water injection part (88K) injection propulsion ship Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してスクリュー(7C)回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, theoretical combustion chamber (4Y) aiming for increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) is driven as ultra high pressure fuel combustion and screw (7C) rotary oxygen combined water injection unit (88K) injection propulsion Various energy storage cycle coalescence engines and coalescence methods for driving a ship. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) Super-high pressure fuel combustion 1 to multiple drives of the theoretical expansion engine (3P) and multiple rotations of the screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving oxygen coalescence water injection part (88K) injection propulsion ship. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drive as a high pressure fuel combustion screw (7C) multiple rotation oxygen combined water injection unit (88K) injection Various energy storage cycle coalescence engines and coalescence methods for driving propulsion vessels. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims at increased combustion of oxygen and hydrogen (4Y) 1 to a plurality of theoretical expansion engines (3P) as a super-high pressure fuel combustion and a screw (7C) multi-rotation oxygen combined water injection unit ( 88K) Various energy storage cycle coalescence engine and coalescence method for driving a propulsion propulsion ship. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進酸素合体スクリュー噴射船舶(39K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) Super-high pressure fuel combustion 1 to multiple drives of the theoretical expansion engine (3P) and multiple rotations of the screw (7C) Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence water injection section (88K) injection propulsion oxygen coalescence screw injection vessel (39K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進酸素合体スクリュー噴射船舶(39K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drive as a high pressure fuel combustion screw (7C) multiple rotation oxygen combined water injection unit (88K) injection Various energy storage cycle coalescence engine and coalescence method for driving propulsion oxygen coalescence screw injection ship (39K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してスクリュー(7C)複数回転酸素合体水噴射部(88K)噴射推進酸素合体スクリュー噴射船舶(39K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims at increased combustion of oxygen and hydrogen (4Y) 1 to a plurality of theoretical expansion engines (3P) as a super-high pressure fuel combustion and a screw (7C) multi-rotation oxygen combined water injection unit ( 88K) Various types of energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence screw injection vessel (39K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動して酸素合体水噴射部(88K)噴射推進酸素合体スクリュー噴射船舶(39K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming to increase combustion of oxygen and hydrogen to a compression volume of 21/60000 of air compression and driving the theoretical expansion engine (3P) as super high pressure fuel combustion and oxygen combined water injection part (88K) injection Various energy storage cycle coalescence engine and coalescence method for driving propulsion oxygen coalescence screw injection ship (39K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that aims to increase the compression volume to 21/60000 of the air compression and aim to increase combustion The oxygen combined water injection part (88K) injection propulsion ship driven by multiple ultrahigh pressure fuel combustion injection propulsion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen hydrogen (4Y) Oxygen coalescence water injection unit (88K) injection propulsion and various energy storage cycle coalescence engine and coalescence method . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and promotes streamline oxygen-hydrogen augmentation combustion (4Y) Oxygen coalescence water injection unit (88K) with multiple ultrahigh pressure fuel combustion injection propulsion Various energy conservation cycle coalescence engines that drive ships And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Oxygen combined water injection unit (88K) with a multi-high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Y) air suction passage aiming at a streamline type oxygen hydrogen increase combustion aiming at a compression volume of 21/60000 of air compression ) Various energy storage cycle coalescing engines and coalescence methods for driving jet propulsion vessels. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with streamline oxyhydrogen by receiving electricity + Oxygen combined water injection part (88K) injection propulsion including multi-high pressure fuel combustion injection propulsion equipped with air suction passage Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進船舶駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam received, theoretical combustion chamber (4Y) aiming at streamline oxyhydrogen increase combustion, oxygen combined water injection part (88K) injection propulsion ship equipped with multiple ultra high pressure fuel combustion injection propulsion equipped with air suction channel Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進酸素合体噴射船舶(39J)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Oxygen combined water injection unit (88K) with a multi-high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Y) air suction passage aiming at a streamline type oxygen hydrogen increase combustion aiming at a compression volume of 21/60000 of air compression ) Various types of energy storage cycle coalescence engine and coalescence method for driving an injection propulsion oxygen coalescence injection ship (39J). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進酸素合体噴射船舶(39J)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at streamline oxygen hydrogen augmentation combustion (4Y) Oxygen coalescence water injection part (88K) jet propulsion oxygen coalescence injection ship (39J) ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88K)噴射推進酸素合体噴射船舶(39J)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electrical + Superheated steam receiving theoretical flow chamber (4Y) with oxygen suction and oxygen superposition fuel injection unit (88K) injection propulsion oxygen coalescence injection Various energy storage cycle coalescence engine and coalescence method for driving a ship (39J). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数とした酸素合体水噴射部(88K)噴射推進酸素合体噴射船舶(39J)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And a compressed combustion chamber (4Y) with a plurality of theoretical combustion chambers (4Y) aiming to increase the compression volume of air compression to 21/60000 of air compression The oxygen coalescence water injection part (88K) injection propulsion oxygen coalescence injection ship (39J) is driven Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that aims to increase the compression volume of air compression to 21/60000 of the air compression aiming at the combustion chamber (4Y) oxygen combined air injection unit (88A) injection propulsion airplane with multiple ultrahigh pressure fuel combustion injection propulsion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at streamline type oxygen-hydrogen augmentation combustion (4Y) Oxygen coalescence air injection part (88A) in which multiple ultrahigh pressure fuel combustion injection propulsion propulsion and various energy storage cycle coalescence engine and coalescence method . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electrical + Superheated steam is received, theoretical combustion chamber (4Y) aiming at streamline oxygen hydrogen augmentation combustion, oxygen combined air injection unit (88A) with multiple super high pressure fuel combustion injection propulsion And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Oxygen combined air injection unit (88A) with a plurality of super high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Y) air suction flow path aiming at increased combustion of streamline oxyhydrogen to reduce compression volume to 21/60000 of air compression ) Various energy conservation cycle coalescence engines and coalescence methods for making jet propulsion airplanes. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at streamline oxygen-hydrogen augmentation combustion (4Y) Oxygen combined air injection part (88A) injection propulsion airplane equipped with multiple ultrahigh pressure fuel combustion injection propulsion including various types of energy storage Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進飛行機にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam received, theoretical combustion chamber (4Y) aiming at increased combustion of oxygen-hydrogen hydrogen, and oxygen combined air injection part (88A) injection propulsion airplane with multiple ultrahigh pressure fuel combustion injection propulsion including air suction flow path Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進酸素合体噴射飛行機(39L)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Oxygen combined air injection unit (88A) with a plurality of super high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Y) air suction flow path aiming at increased combustion of streamline oxyhydrogen to reduce compression volume to 21/60000 of air compression ) Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion oxygen coalescence airplane (39L). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進酸素合体噴射飛行機(39L)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen-hydrogen hydrogen (4Y) The oxygen coalescence air injection part (88A) injection propulsion oxygen coalescence injection plane (39L) that includes the air suction flow path ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、流線型酸素水素増大燃焼狙う理論燃焼室(4Y)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進とした酸素合体空気噴射部(88A)噴射推進酸素合体噴射飛行機(39L)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Oxygen combined air injection part (88A) injection propulsion oxygen combined injection including theoretical combustion chamber (4Y) air suction flow path that receives + electricity + superheated steam and aims at streamline oxygen hydrogen augmentation combustion Various energy storage cycle coalescence engine and coalescence method for driving an airplane (39L). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする流線型酸素水素増大燃焼狙う理論燃焼室(4Y)複数とした酸素合体空気噴射部(88A)噴射推進酸素合体噴射飛行機(39L)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And a compressed combustion chamber (4Y) with a plurality of theoretical combustion chambers (4Y) aiming to increase the compression volume to 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してプロペラ(7A)回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) Driven by a theoretical expansion engine (3P) as an ultrahigh pressure fuel combustion and driven by a propeller (7A) rotating airplane Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してプロペラ(7A)回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Various energy storage cycle coalescence engines and coalescence methods that drive a theoretical expansion engine (3P) and drive a propeller (7A) as an ultra-high pressure fuel combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してプロペラ(7A)回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production A theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims at increased combustion of oxygen and hydrogen (4Y) as an ultrahigh pressure fuel combustion, drives a theoretical expansion engine (3P), and propellers (7A) various energy storage cycle combined engines that drive a rotating airplane, and Merge method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) As a super-high pressure fuel combustion, the theoretical expansion engine (3P) 1 is driven multiple times and the propeller (7A) is rotated multiple times. Various energy storage cycle coalescence engine and coalescence method for driving an airplane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drive and propeller (7A) various energy storage cycle coalescing engine as ultra high pressure fuel combustion And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Receiving superheated steam, theoretical combustion chamber (4Y) aiming to increase combustion with oxygen and hydrogen (4Y) Theoretically expanding engine (3P) 1 to multiple drives and propeller (7A) to drive multiple revolution airplanes as ultra high pressure fuel combustion Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転酸素合体プロペラ飛行機(39M)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression. (4Y) As a super-high pressure fuel combustion, the theoretical expansion engine (3P) 1 is driven multiple times and the propeller (7A) is rotated multiple times. Various energy storage cycle merging engines and merging methods driven by an oxygen merging propeller airplane (39M). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転酸素合体プロペラ飛行機(39M)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen by receiving electricity and driving the theoretical expansion engine (3P) 1 to multiple propellers (7A) and multi-rotation oxygen combined propeller plane (39M) as ultra high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動してプロペラ(7A)複数回転酸素合体プロペラ飛行機(39M)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electrical + Superheated steam is received, theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple driving propeller (7A) multi-rotation oxygen combined propeller airplane (39M ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動してプロペラ(7A)回転酸素合体プロペラ飛行機(39M)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen with a compression volume of 21/60000 of air compression and driving the theoretical expansion engine (3P) as an ultra-high pressure fuel combustion propeller (7A) rotating oxygen combined propeller airplane (39M) Various energy storage cycle merging engines and merging methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動回転翼(7B)回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to achieve a compression volume of 21/60000 of air compression (4Y) Theoretical expansion engine (3P) driven rotor blade (7B) rotates as an ultra-high pressure fuel combustion to drive the airplane Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動回転翼(7B)回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) driven rotor blade (7B) as an ultra-high pressure fuel combustion . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動回転翼(7B)回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and increases oxygen and hydrogen combustion and aims at high-pressure fuel combustion Theoretical expansion engine (3P) Drive rotor (7B) And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression (4Y) Theoretical expansion engine (3P) 1 to the multi-drive rotor blade (7B) multiple rotations as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods that drive aircraft. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims to increase combustion with oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1-Multi-drive rotor (7B) Various energy storage cycles combined to drive the aircraft by multiple rotations Organization and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam by receiving electricity + superheated steam and aims at increased combustion of oxygen and hydrogen. Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して酸素合体回転翼飛行機(39P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression (4Y) Theoretical expansion engine (3P) 1 to the multi-drive rotor blade (7B) multiple rotations as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods that drive oxygen coalesced rotorcraft (39P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して酸素合体回転翼飛行機(39P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims to increase combustion with oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drive rotors (7B) as an ultra-high pressure fuel combustion and oxygen combined rotor blade airplane (39P) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動回転翼(7B)複数回転して酸素合体回転翼飛行機(39P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims to increase combustion with oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 to multiple drive rotor (7B) as oxygen combustion rotor blade (39P) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動回転翼(7B)回転して酸素合体回転翼飛行機(39P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) Ultrahigh pressure fuel combustion Theoretical expansion engine (3P) The rotating rotor blade (7B) rotates to rotate the oxygen combined Various energy storage cycle coalescence engine and coalescence method for driving a wing airplane (39P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動プロペラ(7A)回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that aims to increase combustion of oxygen and hydrogen to make the compression volume 21/60000 of air compression aims at the combustion chamber (4Y) ultrahigh pressure fuel combustion and the theoretical expansion engine (3P) drive propeller (7A) rotates and the oxygen combined air injection unit (88A) Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion airplane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動プロペラ(7A)回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) A high-pressure fuel combustion Theoretical expansion engine (3P) drive propeller (7A) rotates and the oxygen combined air injection part (88A) injection propulsion airplane drives Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動プロペラ(7A)回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam receiving theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) drive propeller (7A) rotates as an ultra-high pressure fuel combustion and oxygen combined air injection part (88A) injection propulsion airplane Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) Theoretical expansion engine (3P) 1-multiple drive propeller (7A) multiple rotations as super high pressure fuel combustion Combined air injection unit (88A) Various energy storage cycle combined engines and combined methods for driving an injection propulsion airplane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at oxygen-hydrogen-enhanced combustion (4Y) Theoretical expansion engine (3P) 1-multiple drive propeller (7A) multiple rotations and oxygen combined air injection part (88A) injection propulsion Various energy storage cycle coalescence engine and coalescence method for driving an airplane. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進飛行機駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, theoretical combustion chamber (4Y) aiming for increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 -multiple drive propeller (7A) multiple rotations and oxygen combined air injection unit (88A) ) Various energy storage cycle coalescence engines and coalescence methods for driving jet propulsion airplanes. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進酸素合体プロペラ噴射飛行機(39N)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) Theoretical expansion engine (3P) 1-multiple drive propeller (7A) multiple rotations as super high pressure fuel combustion Combined air injection unit (88A) injection propulsion oxygen combination propeller injection plane (39N) various energy storage cycle combination engine and combination method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進酸素合体プロペラ噴射飛行機(39N)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at oxygen-hydrogen-enhanced combustion (4Y) Theoretical expansion engine (3P) 1-multiple drive propeller (7A) multiple rotations and oxygen combined air injection part (88A) injection propulsion Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence propeller jet airplane (39N). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88A)噴射推進酸素合体プロペラ噴射飛行機(39N)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, theoretical combustion chamber (4Y) aiming for increased combustion of oxygen and hydrogen (4Y) Theoretical expansion engine (3P) 1 -multiple drive propeller (7A) multiple rotations and oxygen combined air injection unit (88A) ) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence propeller jet airplane (39N). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として理論膨張機関(3P)駆動プロペラ(7A)回転し酸素合体空気噴射部(88A)噴射推進酸素合体プロペラ噴射飛行機(39N)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that aims to increase combustion of oxygen and hydrogen to make the compression volume 21/60000 of air compression aims at the combustion chamber (4Y) ultrahigh pressure fuel combustion and the theoretical expansion engine (3P) drive propeller (7A) rotates and the oxygen combined air injection unit (88A) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence propeller jet airplane (39N). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production From the high pressure high temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as a theoretical combustion chamber (4Y) super high pressure fuel combustion aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression Various energy storage cycle coalescence engine and coalescence method in which high pressure and high temperature combustion gas (50) is injected to drive a theoretical expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) High pressure high temperature combustion gas control valve (5a) High pressure high temperature combustion gas (50) is injected from the open combustion gas injection nozzle (6Y) Various energy storage cycle coalescence engines and coalescence methods that drive a theoretical expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and increases oxygen and hydrogen combustion, and serves as a high-pressure high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as an ultra-high pressure fuel combustion (50) ) To drive a theoretical expansion engine (3P) and various energy storage cycle coalescing engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転する理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production From the high pressure high temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as a theoretical combustion chamber (4Y) super high pressure fuel combustion aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression Various energy storage cycle coalescence engine and coalescence which drive a theoretical expansion engine (3P) which injects high-pressure and high-temperature combustion gas (50) to rotate the upper expansion blade (8d) and lower expansion blade (8e) horizontally (1h) Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転する理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) High pressure high temperature combustion gas control valve (5a) High pressure high temperature combustion gas (50) is injected from the open combustion gas injection nozzle (6Y) Then, various energy storage cycle coalescing engines and coalescence methods for driving the theoretical expansion engine (3P) in which the upper expansion blade (8d) and the lower expansion blade (8e) are reversed in the horizontal axis (1h). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転する理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and increases oxygen and hydrogen combustion, and serves as a high-pressure high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as an ultra-high pressure fuel combustion (50) ) To inject the upper expansion wing (8d) and the lower expansion wing (8e) into the horizontal axis (1h) and to reverse the theoretical expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転組立タービン翼(8f)組立の理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production From the high pressure high temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as a theoretical combustion chamber (4Y) super high pressure fuel combustion aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression Various types of driving high-pressure high-temperature combustion gas (50) to drive the upper expansion blade (8d) and the lower expansion blade (8e) to the horizontal expansion shaft (1h), the counter-rotating assembly turbine blade (8f), and the theoretical expansion engine (3P). Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転組立タービン翼(8f)組立の理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at increased combustion of oxygen and hydrogen (4Y) High pressure high temperature combustion gas control valve (5a) High pressure high temperature combustion gas (50) is injected from the open combustion gas injection nozzle (6Y) Then, various energy storage cycle coalescence engines and coalescence methods for driving the upper expansion blade (8d) and the lower expansion blade (8e) to the theoretical expansion engine (3P) of the horizontal axis (1h) counter rotating assembly turbine blade (8f) assembly. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転組立タービン翼(8f)組立の理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and increases oxygen and hydrogen combustion, and serves as a high-pressure high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y) as an ultra-high pressure fuel combustion (50) ) To drive the upper expansion blade (8d) and the lower expansion blade (8e) to the horizontal expansion shaft (1h), the counter-rotating assembly turbine blade (8f), the theoretical expansion engine (3P), Merge method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放空気吸引燃焼量増大し、燃焼ガス噴射ノズル(6Y)より高圧高温燃焼ガス(50)を噴射して上側膨張翼(8d)下側膨張翼(8e)を横軸(1h)二重反転組立タービン翼(8f)組立の理論膨張機関(3P)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) High-pressure high-temperature combustion gas control valve (5a) Increases open air suction combustion amount and combustion The high-pressure high-temperature combustion gas (50) is injected from the gas injection nozzle (6Y), and the upper expansion blade (8d) and the lower expansion blade (8e) are turned on the horizontal axis (1h). Various energy storage cycle coalescence engines and coalescence methods driven by an engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張する理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression. (4Y) High-pressure high-temperature combustion gas control valve (5a) expands and expands 380 degrees in the circumferential direction as ultrahigh-pressure fuel combustion Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張する理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims to increase combustion with oxygen and hydrogen (4Y) Various types of high-pressure high-temperature combustion gas control valve (5a) open the theoretical expansion engine (3P) that expands and expands 380 degrees in the circumferential direction Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張する理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims to increase combustion with oxygen and hydrogen (4Y) The high-pressure and high-temperature combustion gas control valve (5a) as the ultrahigh-pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to reduce the compression volume to 21/60000 of air compression. (4Y) High pressure high temperature combustion gas control valve (5a) as an ultra high pressure fuel combustion. Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P) for maximum driving speed. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives electricity and aims at oxygen-hydrogen-enhanced combustion (4Y) High-pressure high-temperature combustion gas control valve (5a) Theoretical expansion engine (maximum driving speed by 380 degrees expansion expansion in the circumferential direction) 3P) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) that receives + electricity + superheated steam and aims at increased combustion of oxygen and hydrogen (4Y) The high pressure and high temperature combustion gas control valve (5a) as an ultra-high pressure fuel combustion Various energy storage cycle coalescing engine and coalescence method for an expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張と二重反転で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression, and the high pressure high temperature combustion gas control valve (5a) as the ultra high pressure fuel combustion. Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3P) that achieves maximum driving speed with counter rotation. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張と二重反転で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) aiming to increase combustion with oxygen and hydrogen by receiving electricity and high-pressure high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion to the maximum driving speed by 380 degrees expansion and double reversal in the circumferential direction Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張と二重反転で最大駆動速度にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that receives superheated steam and receives oxygen and hydrogen-enhanced combustion (4Y) High-pressure high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P) to speed. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする酸素水素増大燃焼狙う理論燃焼室(4Y)超高圧燃料燃焼として高圧高温燃焼ガス制御弁(5a)開放円周方向380度拡大膨張と二重反転にする理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to make the compression volume 21/60000 of the air compression, and the high pressure high temperature combustion gas control valve (5a) as the ultra high pressure fuel combustion. Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P) to be counter-rotated. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、液体燃料(1c)や水(52a)と共に液体圧縮し、圧縮容積を空気圧縮の21/60000容積等で超高圧圧縮燃料噴射燃焼する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion for compressing the liquid together with the liquid fuel (1c) and water (52a), and compressing the compressed volume with an air compression of 21/60000 volume, etc. Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮し、圧縮容積を空気圧縮の21/60000容積等で超高圧圧縮燃料噴射燃焼する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber that receives electricity, compresses liquid together with liquid fuel (1c) and water (52a), and compresses the compressed volume by 21/60000 volume of air compression, etc. 4Y) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮し、圧縮容積を空気圧縮の21/60000容積等で超高圧圧縮燃料噴射燃焼する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and compressed with liquid fuel (1c) and water (52a), and the compression volume is 21 / 60,000 volume of air compression, etc. Various energy storage cycle coalescing engine and coalescence method for the combustion chamber (4Y). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Are combined with liquid fuel (1c) and water (52a) and heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen, and various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive electricity, compress liquid together with liquid fuel (1c) and water (52a), and heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam, various energy storage cycle coalescing engines that heat to the optimum temperature at the inner wall of the theoretical combustion chamber (4Y) aiming to increase combustion with oxygen and hydrogen by liquid compression with liquid fuel (1c) and water (52a), and Merge method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The oxygen control valve (24D) + fuel control valve (25b) is heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Y) for liquid combustion (1c) and water (52a) and compressing the liquid together with the liquid fuel (1c) and water (52a). + Various energy storage cycle coalescence engine and coalescence method for opening the superheated steam control valve (25). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Heated oxygen control valve (24D) + Fuel control valve (+) at the inner wall of the theoretical combustion chamber (4Y) that receives electricity and compresses liquid together with liquid fuel (1c) and water (52a) and aims to increase combustion with oxygen and hydrogen 25b) + various energy storage cycle coalescence engines and coalescence methods that open the superheated steam control valve (25). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam received and compressed with liquid fuel (1c) and water (52a) to increase oxygen hydrogen hydrogen combustion aiming at the inner wall of the theoretical combustion chamber (4Y) heated oxygen control valve (24D) + fuel Various energy storage cycle coalescence engines and coalescence methods for opening the control valve (25b) + superheated steam control valve (25). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して酸素水素増大燃焼狙う理論燃焼室(4Y)内壁で最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放受給過熱蒸気と共に噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Heated oxygen control valve (24D) + fuel control valve to the optimum temperature at the inner wall of the theoretical combustion chamber (4Y) that receives superheated steam and compresses liquid together with liquid fuel (1c) and water (52a) and aims to increase combustion with oxygen and hydrogen (25b) + Various energy storage cycle coalescence engine and coalescence method for injecting the superheated steam control valve (25) together with the open receiving superheated steam. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescing engine and coalescence method for a theoretical combustion chamber (4Y) aimed at oxygen-hydrogen augmentation combustion to be heated. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is opened to the optimum temperature and the outer superheated steam (50 ) To heat the oxygen-hydrogen-enhanced combustion aiming at a theoretical combustion chamber (4Y) and various energy storage cycle coalescing engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱する酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is heated to the optimum temperature. Various energy storage cycle coalescing engine and coalescence method for a theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion for heating steam (50). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescence engines and coalescence methods in which a part of the heating is made into a theoretical combustion chamber (4Y) aimed at oxygen-hydrogen-enhanced combustion aiming at suction pyrolysis electrolysis near the center. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is opened to the optimum temperature and the outer superheated steam (50 ) Various energy storage cycle coalescence engine and coalescence method to make a theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion aiming at suction pyrolysis electrolysis near the center of heating. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is heated to the optimum temperature. Various energy storage cycle coalescing engines and coalescence methods for making steam (50) a theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion aiming at heat pyrolysis electrolysis in the vicinity of the center of heating (50). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescence engines and coalescence methods in which a part of the heating is made into a theoretical combustion chamber (4Y) aiming at oxygen-hydrogen augmentation combustion aiming at suction pyrolysis electrolysis oxygen-hydrogen increase combustion near the center. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is opened to the optimum temperature and the outer superheated steam (50 ) Various energy storage cycle coalescence engine and coalescence method in which a part of the heating is made into a theoretical combustion chamber (4Y) aimed at oxygen pyrolysis electrolysis and oxygen hydrogen augmentation combustion aiming at the vicinity of the center. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) is heated to the optimum temperature. Various energy storage cycle coalescence engine and coalescence method in which steam (50) is heated to a theoretical combustion chamber (4Y) aimed at oxygen pyrolysis electrolysis and oxygen hydrogen augmentation combustion aiming at a part of the heating near the center. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、最適温度に加熱酸素制御弁(24D)+燃料制御弁(25b)+過熱蒸気制御弁(25)を開放酸素燃料バーナー中心付近複数3000℃以上燃焼で受給過熱蒸気含む外周過熱蒸気(50)を加熱一部を中心付近に吸引熱分解電気分解酸素水素増大燃焼狙う酸素水素増大燃焼狙う理論燃焼室(4Y)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Receiving superheated steam, heating oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature including overheated steam received at a temperature of 3000 ° C. or more near the open oxygen fuel burner center Various energy storage cycle coalescence engines and coalescence methods for heating the peripheral superheated steam (50) to a theoretical combustion chamber (4Y) aiming at oxygen pyrolysis electrolysis oxygen hydrogen augmentation combustion aiming at a part of heating near the center. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And a combination of various energy conservation cycle coalescence engines and coalescence with a combustion gas (49) injection accelerating injection oxygen merging water injection part (88K) comprising a plurality of series of theoretical combustion chambers (4Y) aiming to increase combustion with oxygen and hydrogen. Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Energy storage cycle coalescence engine that receives electricity and has a theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion as a streamlined combustion gas (49) oxygen merging water injection part (88K) for accelerated injection And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, and the theoretical combustion chamber (4Y) aiming at oxygen-hydrogen augmentation combustion is streamlined. Combustion gas with multiple series (49) Oxygen combined water injection part (88K) of accelerated injection is stored. Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The combustion chamber (4) is equipped with multiple theoretical combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion and has a series of combustion gases (49) (4Y) Oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88K) to be used by heating. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen by receiving electricity, and has a streamlined combustion gas (49) with a series of combustion gases (49) (4Y) oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) used by heating at an optimum temperature. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and the combustion chamber (4Y) with a plurality of in-line combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion is provided in series (4Y) Oxygen + fuel on the inner wall (4Y) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) that uses superheated steam heated at an optimum temperature. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The combustion chamber (4) is equipped with multiple theoretical combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion and has a series of combustion gases (49) (4Y) Oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88K) that is heated to produce a theoretical combustion chamber (4Y) combustion or the like aiming at increased oxygen-hydrogen combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen by receiving electricity, and has a streamlined combustion gas (49) with a series of combustion gases (49) (4Y) oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88K) that is heated to an optimal temperature to make a theoretical combustion chamber (4Y) combustion aiming at oxygen-hydrogen-enhanced combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and the combustion chamber (4Y) with a plurality of in-line combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion is provided in series (4Y) Oxygen + fuel on the inner wall (4Y) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) for heating the superheated steam at an optimal temperature to make a combustion chamber (4Y) combustion aiming at increased oxygen hydrogen combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+受給加熱蒸気を含む過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Thermal combustion chamber (4Y) that receives superheated steam and aims at oxygen-hydrogen-enhanced combustion is streamlined. Combustion gas (49) is provided in series with (4Y) inner wall and combustion flow inner wall (5d) oxygen + fuel + receiving heating Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88K) for heating a superheated steam containing steam to an optimal combustion chamber (4Y) combustion aiming at oxygen-hydrogen-enhanced combustion by optimal temperature heating. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods with a targeted oxygen coalescence water injection section (88K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) near the center where oxygen is received and electricity + oxygen + fuel + superheated steam is heated at the optimal temperature on each inner wall to aim for increased combustion of oxygen and hydrogen (4Y) Overheated steam suction pyrolysis by combustion above 3000 ° C Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) aimed at electrolysis. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the target is a theoretical combustion chamber (4Y) near the center to increase combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence water injection unit (88K) aimed at suction pyrolysis electrolysis. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) aimed at oxygen-hydrogen augmentation combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) near the center where oxygen is received and electricity + oxygen + fuel + superheated steam is heated at the optimal temperature on each inner wall to aim for increased combustion of oxygen and hydrogen (4Y) Overheated steam suction pyrolysis by combustion above 3000 ° C Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88K) aimed at electrolysis oxygen hydrogen augmentation combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the target is a theoretical combustion chamber (4Y) near the center to increase combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence water injection unit (88K) aimed at increased combustion by suction pyrolysis electrolysis oxygen hydrogen. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88K) for heating and injecting superheated steam (50) of the superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to increase the combustion temperature inner wall (5d) ) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence water injection part (88K) for heating and injecting superheated steam (50) in the outer peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel on each inner wall + Superheated steam is heated to the optimum temperature, and the target is a theoretical combustion chamber (4Y) near the center. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88K) for heating and injecting superheated steam (50) in the inner wall (5d) outer peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の受給過熱蒸気を含む過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Receiving superheated steam, oxygen + fuel on each inner wall + heated superheated steam at optimum temperature and aiming to increase combustion of oxygen hydrogen hydrogen near the center (4Y) near the center oxygen fuel burner Combustion flow inner wall (more than 3000 ° C combustion) 5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injecting section (88K) for heating and injecting superheated steam (50) including the received superheated steam in the outer peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycles using an oxygen combined water injection unit (88K) that also performs combustion injection in the same manner as the theoretical combustion chamber (4Y) having a plurality of streamline-type oxygen-hydrogen-enhancing combustion targets at the optimum location of air (28a) suction injection flow Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity received in the air (28a) optimum injection point of the air (28a) A plurality of streamline type oxygen hydrogen increased combustion aimed at the theoretical combustion chamber (4Y) Various energy made into the oxygen combined water injection part (88K) in the same way combustion injection Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体水噴射部(88K)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electrical + Superheated steam is received, and the oxygen (28a) suction injection flow optimal location is also equipped with a plurality of streamline type oxygen-hydrogen-enhancing combustion combustion chambers (4Y). Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大した各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The various energy storage cycle coalescence engine and coalescence method which expanded the air inlet to the oxygen coalescence water injection part (88K). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大した各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive electricity and use an oxygen coalescence water injection section (88K) to expand the air inlet forward. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大した各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Energy storage cycle coalescence engine and coalescence method which received + electricity + superheated steam and made the oxygen coalescence water injection part (88K) expand the air inlet forward. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大して直線に近付けて船底に気泡最大噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods, in which an oxygen coalescence water injection unit (88K) is used to enlarge the air inlet toward the straight line to bring it into a straight line and inject the maximum amount of bubbles to the ship bottom. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大して直線に近付けて船底に気泡最大噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive electricity, make the oxygen coalescence water injection section (88K) expand the air inlet forward, approach the straight line, and inject the maximum amount of bubbles to the bottom of the ship. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大して直線に近付けて船底に気泡最大噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods that receive + electricity + superheated steam, make the oxygen coalescence water injection section (88K) expand the air inlet forward, approach the straight line, and inject the bubbles to the bottom of the ship at the maximum. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、酸素合体水噴射部(88K)にして空気入口を前向き拡大して直線に近付けて船底に気泡最大噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive superheated steam, use an oxygen coalescence water injection unit (88K), expand the air inlet forward, approach the straight line, and inject maximum bubbles into the ship bottom. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production And a combination of various energy conservation cycle coalescence engines and coalescence with a combustion chamber (49) with an oxygen merging air injection part (88A) for accelerating injection with a plurality of series of theoretical combustion chambers (4Y) aiming to increase combustion with oxygen and hydrogen. Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Energy storage cycle coalescence engine that receives electricity, and has a theoretical combustion chamber (4Y) aiming at oxygen-oxygen-enhanced combustion as a streamlined combustion gas (49) and an oxygen coalescence air injection part (88A) for accelerated injection And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)噴射加速噴射の酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and the theoretical combustion chamber (4Y) aiming at oxygen-hydrogen-enhanced combustion is streamlined. Combustion gas (49) injection-accelerated injection oxygen-combined air injection unit (88A) is provided in series. Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The combustion chamber (4) is equipped with multiple theoretical combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion and has a series of combustion gases (49) (4Y) Oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) to be used by heating. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen by receiving electricity, and has a streamlined combustion gas (49) with a series of combustion gases (49) (4Y) oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) used by heating at an optimum temperature. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して使用する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and the combustion chamber (4Y) with a plurality of in-line combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion is provided in series (4Y) Oxygen + fuel on the inner wall (4Y) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88A) that uses superheated steam heated at an optimum temperature. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The combustion chamber (4) is equipped with multiple theoretical combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion and has a series of combustion gases (49) (4Y) Oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalesced air injection section (88A) that are heated and used for the theoretical combustion chamber (4Y) combustion or the like aiming at increased oxygen-hydrogen combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) that aims to increase combustion with oxygen and hydrogen by receiving electricity, and has a streamlined combustion gas (49) with a series of combustion gases (49) (4Y) oxygen + fuel + superheated steam on the inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence air injection section (88A) for the theoretical combustion chamber (4Y) combustion or the like aiming at oxygen-hydrogen-enhanced combustion by heating at an optimum temperature. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and the combustion chamber (4Y) with a plurality of in-line combustion chambers (4Y) aiming at oxygen-hydrogen-enhanced combustion is provided in series (4Y) Oxygen + fuel on the inner wall (4Y) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88A) for heating the superheated steam to an optimal temperature to achieve combustion with increased theoretical hydrogen chamber (4Y) aiming at increased oxygen-hydrogen combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、酸素水素増大燃焼狙う理論燃焼室(4Y)を流線型として複数直列具備の燃焼ガス(49)で(4Y)内壁や燃焼流内壁(5d)の酸素+燃料+受給加熱蒸気を含む過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)燃焼等にする酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Thermal combustion chamber (4Y) that receives superheated steam and aims at oxygen-hydrogen-enhanced combustion is streamlined. Combustion gas (49) is provided in series with (4Y) inner wall and combustion flow inner wall (5d) oxygen + fuel + receiving heating Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) for heating a superheated steam containing steam to a theoretical combustion chamber (4Y) combustion aiming at oxygen-hydrogen-enhanced combustion by optimum temperature heating. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescing engines and coalescence methods in the target oxygen coalescence air injection section (88A). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) near the center where oxygen is received and electricity + oxygen + fuel + superheated steam is heated at the optimal temperature on each inner wall to aim for increased combustion of oxygen and hydrogen (4Y) Overheated steam suction pyrolysis by combustion above 3000 ° C Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88A) aimed at electrolysis. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the target is a theoretical combustion chamber (4Y) near the center to increase combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) aimed at suction pyrolysis electrolysis. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence air injection unit (88A) aimed at oxygen-hydrogen augmentation combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Theoretical combustion chamber (4Y) near the center where oxygen is received and electricity + oxygen + fuel + superheated steam is heated at the optimal temperature on each inner wall to aim for increased combustion of oxygen and hydrogen (4Y) Overheated steam suction pyrolysis by combustion above 3000 ° C Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88A) aimed at electrolysis oxygen hydrogen augmentation combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で過熱蒸気吸引熱分解電気分解酸素水素増大燃焼狙いの酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the target is a theoretical combustion chamber (4Y) near the center to increase combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence air injection unit (88A) aimed at increased combustion by suction pyrolysis electrolysis oxygen hydrogen. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Theoretical combustion chamber (4Y) near the center where oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at increased combustion of oxygen and hydrogen. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) for heating and injecting superheated steam (50) in the superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Y) aiming at increased combustion of oxygen and hydrogen to increase the combustion temperature inner wall (5d) ) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence air injection section (88A) for heating and injecting the superheated steam (50) in the peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received, oxygen + fuel on each inner wall + Superheated steam is heated to the optimum temperature, and the target is a theoretical combustion chamber (4Y) near the center. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88A) for heating and injecting superheated steam (50) in the inner wall (5d) outer peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して酸素水素増大燃焼狙う理論燃焼室(4Y)中心付近酸素燃料バーナー複数3000℃以上燃焼で燃焼流内壁(5d)外周過熱蒸気溜(95c)の受給過熱蒸気を含む過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Receiving superheated steam, oxygen + fuel on each inner wall + heated superheated steam at optimum temperature and aiming to increase combustion of oxygen hydrogen hydrogen near the center (4Y) near the center oxygen fuel burner Combustion flow inner wall (more than 3000 ° C combustion) 5d) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence air injection section (88A) for heating and injecting superheated steam (50) including the received superheated steam in the outer peripheral superheated steam reservoir (95c). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycles using an oxygen combined air injection unit (88A) that also performs combustion injection in the same manner as the theoretical combustion chamber (4Y) having a plurality of streamline type oxygen-hydrogen-enhanced combustion aiming at the optimum place of the suction injection flow of air (28a) Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity received in the air (28a) suction injection flow optimum location in the oxygen combustion air injection unit (88A) that also has a plurality of streamline type oxygen hydrogen hydrogen combustion combustion aiming combustion combustion (4Y) as well as various oxygen energy Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型酸素水素増大燃焼狙う理論燃焼室(4Y)具備同様に燃焼噴射する酸素合体空気噴射部(88A)にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electrical + Superheated steam is received, and the oxygen (28a) suction injection flow optimal location is also provided with a plurality of streamline type oxygen hydrogen increased combustion aiming in the theoretical combustion chamber (4Y). Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素合体空気噴射部(88A)を回転して垂直上昇降下を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods that enable vertical ascent and descent by rotating the oxygen coalescence air injection section (88A). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素合体空気噴射部(88A)を回転して垂直上昇降下を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive electricity and rotate the oxygen coalescence air injection section (88A) to enable vertical ascent and descent. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素合体空気噴射部(88A)を回転して垂直上昇降下を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods that receive + electricity + superheated steam and rotate the oxygen coalescence air injection section (88A) to enable vertical ascent and descent. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給して、酸素合体空気噴射部(88A)を回転して逆噴射を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production , Various energy storage cycle coalescence engines and coalescence methods that enable reverse injection by rotating the oxygen coalescence air injection section (88A). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給して、酸素合体空気噴射部(88A)を回転して逆噴射を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive electricity and rotate the oxygen coalescence air injection section (88A) to enable reverse injection. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給して、酸素合体空気噴射部(88A)を回転して逆噴射を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods that receive + electricity + superheated steam and rotate the oxygen coalescence air injection section (88A) to enable reverse injection. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給して、酸素合体空気噴射部(88A)を回転して逆噴射を可能にした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods that receive superheated steam and rotate the oxygen coalescence air injection section (88A) to enable reverse injection. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)とした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b), the energy storage cycle coalescence engine and the coalescence method as an electrically driven theoretical gas compressor (3T) in which the gas volume is compressed from the outer peripheral long large compression wing to the central short compression wing with the gas volume inversely proportional to the pressure. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)とした各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 , Various energy storage cycle coalescence engines and coalescence methods as an electrically driven theoretical gas compressor (3T) that compresses a gas volume from an outer peripheral long compression blade whose center is inversely proportional to pressure to a central short compression blade. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)とした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Various energy storage cycle coalescence engines and coalescence methods that are electrically driven theoretical gas compressors (3T) that receive the gas and compress the gas volume from the outer circumferential long large compression blades to the central short compression blades in an inverse proportion to the pressure. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b), an energy driven cycle coalescence engine that sucks and compresses air as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer circumferential large compression blades to the central short compression blades in an inverse proportion to the pressure And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 Various energy storage cycle coalescence engines and coalescence methods for sucking and compressing air as an electrically driven theoretical gas compressor (3T) that compresses a gas volume from an outer peripheral large compression blade, which is aimed at inverse proportion to pressure, to a central short compression blade. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Various energy storage cycle coalescence engines and coalescence methods for receiving and compressing air as an electrically driven theoretical gas compressor (3T) that receives and compresses the gas volume from the outer peripheral long compression blades to the central short compression blades with the gas volume inversely proportional to the pressure . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮熱交換過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b) is received and air is sucked and compressed as heat exchange superheated steam as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blade to the central short compression blade, which is aimed at inversely proportional to the pressure. Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮熱交換過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 As an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression wing, whose gas volume is inversely proportional to the pressure, to the central short compression wing, various energy storage cycle coalescence engines that produce compressed heat exchange superheated steam by sucking air And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮熱交換過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Receiving and compressing the air volume from the outer peripheral large compression blades to the central short compression blades with the gas volume inversely proportional to the pressure. Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮熱交換過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b) + Heat-suppressed heat-exchange superheated steam that receives superheated steam and sucks air as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral large compression blades to the central short compression blades with the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for manufacturing 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b), and a suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that receives a gas volume and compresses it from an outer peripheral large compression blade whose center is inversely proportional to pressure to a central short compression blade ) Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 The superheated steam is produced by the suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blade to the central short compression blade, which is aimed at inversely proportional to the pressure. Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Received air is heated by an intake-compression air compressor (2Y) as an electric-driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blade to the central short compression blade, which is aimed at inversely proportional to the pressure. Various energy storage cycle coalescence engine and coalescence method for producing steam. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b), and a suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that receives a gas volume and compresses it from an outer peripheral large compression blade whose center is inversely proportional to pressure to a central short compression blade ) Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production supply facility (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 The superheated steam is produced by the suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blade to the central short compression blade, which is aimed at inversely proportional to the pressure. Various energy storage cycle coalescence engines and coalescence methods to be supplied to a supply facility (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Received air is heated by an intake-compression air compressor (2Y) as an electric-driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blade to the central short compression blade, which is aimed at inversely proportional to the pressure. Various energy storage cycle coalescence engines and coalescence methods for supplying steam to the production and supply equipment (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b), and a suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that receives a gas volume and compresses it from an outer peripheral large compression blade whose center is inversely proportional to pressure to a central short compression blade ) Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Receiving low-cost electricity from electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-cost power generation electricity production, vertical type moving blade ratio critical material gravity turbine (8N) with magnetic bearing load approaching 0 , As a theoretically driven gas compressor (3T) that compresses the gas volume from the outer peripheral long compression blades to the central short compression blades in inverse proportion to the pressure, compressed air + superheated with a suction compressed air heat exchanger (2Y) Various energy storage cycle coalescence engines and coalescence methods for supplying steam to the production and supply equipment (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetism bearing load approaching 0. Low cost electricity + superheated steam from electricity + liquid air cold heat + superheated steam hot water supply equipment (3D) of extremely cheap electricity generation electricity production Received air is compressed by a suction compressed air heat exchanger (2Y) as an electrically driven theoretical gas compressor (3T) that compresses the gas volume from the outer peripheral large compression blade to the central short compression blade, which is aimed at inverse proportion to the pressure. Various energy storage cycle coalescence engines and coalescence methods for supplying air + superheated steam to manufacturing and supply equipment (3D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価電気+高温水(52b)+過熱蒸気を受給して、気体の体積が圧力に反比例狙いの外周長大圧縮翼から中心短圧縮翼に圧縮する電気駆動の理論気体圧縮機(3T)として空気を吸入圧縮圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気を製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost electricity + high-temperature water (8D), electricity + liquid air cold heat + superheated steam heat supply facility (3D) 52b) + Compressed air heat exchange with suction air as an electrically driven theoretical gas compressor (3T) that receives superheated steam and compresses the gas volume from the outer peripheral large compression wing to the central short compression wing with the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for supplying compressed air + superheated steam to the production supply facility (3D) with the vessel (2Y). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成とした各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods configured to compress from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として空気圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for compressing air as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として空気(28a)圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching 0 The extremely large generator blade with a theoretical gas compressor (3T) of extremely inexpensive power generation and electric drive, with the gas volume complying with the pressure inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) from the outer periphery to the suction center as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮水を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods that heat air (28a) compressed water from the outer periphery to the suction center as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮高温水を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed high-temperature water from the outer periphery to the suction center as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮過熱蒸気を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero (8N) Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) with a gas volume that is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed superheated steam from the outer circumference to the suction center from the outer periphery as a configuration for compression from (8) to the central short compressor blade (8) 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮圧縮空気熱交換器(2Y)で水を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero (8N) Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) with a gas volume that is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods in which water is heated by air (28a) from the outer periphery to the suction center as a configuration to be compressed from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮圧縮空気熱交換器(2Y)で高温水を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero (8) Various energy storage cycle coalescence engines and coalescence methods in which high temperature water is heated by air (28a) compression / compression air heat exchanger (2Y) from the outer periphery to the suction center as a configuration for compression from the outer short compression blade (8) to (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として外周から吸入中心に空気(28a)圧縮圧縮空気熱交換器(2Y)で過熱蒸気を加熱する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for heating superheated steam with air (28a) compression-compression air heat exchanger (2Y) from the outer periphery to the suction center as a configuration for compression from (8) to the central short compression blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で過熱蒸気製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero (8N) Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) with a gas volume that is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam with a compressed air heat exchanger (2Y) as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for producing compressed air + superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で高圧圧縮空気+高圧過熱蒸気製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for producing high-pressure compressed air + high-pressure superheated steam with a compressed air heat exchanger (2Y) as a configuration for compression from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で超高圧圧縮空気+超高圧過熱蒸気製造する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for producing ultra-high pressure compressed air + ultra-high pressure superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で圧縮空気+過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration for compressing from (8) to the central short compressor blade (8). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で高圧圧縮空気+高圧過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engine and coalescence method for supplying high pressure compressed air + high pressure superheated steam production and supply equipment (3D) with compressed air heat exchanger (2Y) as a configuration for compressing from (8) to central short compressor blade (8) . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で超高圧圧縮空気+超高圧過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines that supply the ultra-high pressure compressed air + ultra-high pressure superheated steam production and supply facility (3D) with the compressed air heat exchanger (2Y) as a configuration that compresses from (8) to the central short compressor blade (8); Merge method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で液体空気+超高圧過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engine and coalescence method for supplying liquid air + superhigh pressure superheated steam production / supply facility (3D) with compressed air heat exchanger (2Y) as a configuration for compressing from (8) to central short compressor blade (8) . 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で液体酸素+液体窒素+超高圧過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycle coalescence engines that supply liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration for compression from (8) to the central short compressor blade (8) And coalescing method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気駆動の、理論気体圧縮機(3T)を気体の体積が圧力に反比例遵守として外周長大圧縮翼(8)から中心短圧縮翼(8)に圧縮する構成として圧縮空気熱交換器(2Y)で電気+液体酸素+液体窒素+超高圧過熱蒸気製造供給設備(3D)に供給する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with magnetically approaching bearing load close to zero Various energy storage cycles for supplying electricity + liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration for compression from (8) to the central short compressor blade (8) Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods in which fuel is injected and combusted, and fuel is injected and combusted from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods in which electricity is received and injected by fuel injection, and fuel is injected and combusted from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam is received and injected and burned, and in the expansion process of 380 degrees in the circumferential direction, the fuel pipe (25a) and the extended upper expansion blade group (8d) are fuel-injected and combusted from multiple locations. Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescence engines and coalescence methods that increase the amount of fuel injection combustion combustion from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Energy storage cycle coalescence engine and coalescence that increase the amount of fuel injection combustion combustion from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees in the fuel receiving fuel injection combustion Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam received fuel injection combustion, in the process of expansion 380 degrees in the circumferential direction, the fuel pipe (25a) extended upper expansion blade group (8d) increase the fuel injection combustion combustion amount from multiple locations Combined with various energy conservation cycle Organization and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production Various energy storage cycle coalescing engines and coalescing methods in which the fuel is injected and burned and compressed with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods in which electricity is received and injected and burned, and compressed with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + Superheated steam received fuel injection combustion, various energy storage cycle coalescence engine and coalescence method for compressing air between the turbine outer box (77a) in the circumferential direction 380 degrees expansion process. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Various energy storage cycle coalescence engines and coalescence methods in which superheated steam is received and injected and burned, and compressed with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production The fuel is injected and burned, and in the expansion process of 380 degrees in the circumferential direction, air compression is performed between the upper expansion blade group (8d) and the lower expansion blade group (8e) at a plurality of locations with the turbine outer casing (77a). Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received and injected and burned, and in the expansion process of 380 degrees in the circumferential direction, air compression is performed between the upper outer blade group (8d) and the lower expansion blade group (8e) at a plurality of locations with the turbine outer casing (77a). Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + superheated steam is received and injected and burned, and compressed in the circumferential direction of 380 degrees with the turbine outer casing (77a), respectively, on the upper expansion blade group (8d) and on the lower expansion blade group (8e) Various energy storage cycle coalescence engines and coalescence methods for injecting at multiple locations. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する理論膨張機関(3P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production In the process of expansion of 380 degrees in the circumferential direction, air compression is performed between the upper expansion blade group (8d) and the lower expansion blade group (8e) at a plurality of locations. Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3P) with increasing quantity. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity is received and injected and burned, and in the expansion process of 380 degrees in the circumferential direction, air compression is performed between the upper outer blade group (8d) and the lower expansion blade group (8e) at a plurality of locations with the turbine outer casing (77a). Various energy storage cycle coalescence engines and coalescence methods that increase the amount of fuel combustion. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + superheated steam is received and injected and burned, and compressed in the circumferential direction of 380 degrees with the turbine outer casing (77a), respectively, on the upper expansion blade group (8d) and on the lower expansion blade group (8e) Various energy storage cycle coalescing engines and coalescence methods for increasing the amount of fuel injected at multiple locations. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼し、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production In the process of expansion of 380 degrees in the circumferential direction, fuel is injected and combusted from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d), and compressed with the turbine outer casing (77a). Each of the upper expansion blade group (8d) and the lower expansion blade group (8e), various energy storage cycle coalescence engines and coalescence methods for increasing the amount of fuel injected at a plurality of locations. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼し、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Injection and combustion of fuel by receiving electricity, and fuel injection and combustion from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential direction of 380 degrees expansion, between the turbine outer box (77a) Various types of energy storage cycle coalescence engine and coalescence method for increasing the amount of fuel injected at a plurality of locations, each of the upper compression blade groups (8d) and the lower expansion blade groups (8e). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼し、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Electricity + superheated steam is received and injected and burned, and in the expansion process of 380 degrees in the circumferential direction, fuel is injected and burned from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d), and the turbine outer casing (77a) Various energy storage cycle coalescence engines and coalescence methods for increasing the amount of fuel injected at a plurality of locations between the air compression upper expansion blade group (8d) and lower expansion blade group (8e). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)極端に安価発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+過熱蒸気を受給燃料噴射燃焼して、円周方向380度膨張過程で、燃料管(25a)延長上側膨張翼群(8d)複数個所より燃料噴射燃焼し、タービン外箱(77a)との間で空気圧縮夫々上側膨張翼群(8d)下側膨張翼群(8e)複数個所噴射燃料燃焼量増大する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) approaching zero using magnetism, low-cost liquid oxygen (5K) than electricity + liquid air cold heat + superheated steam heat supply equipment (3D) of extremely low-priced electricity production + Superheated steam is received and injected and burned, and in the process of expansion by 380 degrees in the circumferential direction, the fuel pipe (25a) is extended from the upper expansion blade group (8d), and fuel is injected and burned between the turbine outer box (77a). In the air compression, the upper expansion blade group (8d) and the lower expansion blade group (8e) various energy storage cycle coalescence engines and coalescence methods for increasing the amount of fuel injected at a plurality of locations. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転する磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Cylindrical all-blade ratio critical material gravity turbine (8N) with a magnetic utilization bearing load approaching to zero Various energy storage cycle coalescence engines and coalescence methods for generating power as a turbine utilizing magnetic force that double-rotates the outer blade group (60D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転する磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And an energy storage cycle coalescence engine and a coalescence method for generating power as a turbine utilizing magnetic force that double-inverts a cylindrical outer rotor blade group (60D). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転する磁力利用多数のタービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And energy storage cycle coalescence engine and coalescence method for generating power as a large number of turbines utilizing magnetic force to double-reverse the outer rotor blade group (60D) and the cylindrical outer blade group. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Cylindrical all-blade ratio critical material gravity turbine (8N) with a magnetic utilization bearing load approaching to zero Various energy storage cycle coalescence engines and coalescence methods for generating electricity as a turbine utilizing magnetic force in which the outer rotor blade group (60D) is double-reversed by a double-reversal magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And a cylinder outer rotor blade group (60D) and various energy storage cycle coalescence engines and a coalescence method for generating power as a turbine using magnetic force that is double-reversed by a double reversal magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する磁力利用多数のタービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And an energy storage cycle coalescence engine and a coalescence method for generating electricity as a large number of turbines using magnetic force that double-reverses the outer rotor blade group (60D) and the cylindrical outer rotor group (60D) with a contra-rotating magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する重量支持等磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Cylindrical all-blade ratio critical material gravity turbine (8N) with a magnetic utilization bearing load approaching to zero Various energy storage cycle coalescence engines and coalescence methods for generating electricity as a weight-supported, etc., magnetic force turbine in which the outer rotor blade group (60D) is doubly reversed by the contra-rotating magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する重量支持等磁力利用タービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And an energy storage cycle coalescence engine and a coalescence method for generating power as a weight-supported magnetic force turbine in which the outer rotor blade group (60D) and the cylindrical outer rotor group (60D) are doubly reversed by the contra-rotating magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)真空中超高圧垂直下方に混合噴射含む比重大物質噴射し重力加速度加速して複数の円筒内側動翼群(60C)と円筒外側動翼群(60D)を二重反転磁気装置(85)で二重反転する重量支持等磁力利用多数のタービンとして発電する各種エネルギ保存サイクル合体機関及び合体方法。   Vertically moving blade ratio critical material gravity turbine (8N) with a magnetic bearing load approaching zero (8N) Specific critical material injection including mixed injection vertically under vacuum and acceleration of gravitational acceleration to accelerate multiple cylindrical inner blade groups (60C) And energy storage cycle coalescence engine and coalescence method for generating power as a large number of turbines utilizing a magnetic force such as weight support that reversely reverses the outer rotor blade group (60D) and the cylindrical outer rotor group (60D) with a counter magnetic device (85). 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼+ジェット燃焼として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   All types of energy storage cycle coalescence engine and coalescence driven by oxygen combined water injection unit (88K) as a vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + rocket combustion + jet combustion with magnetic bearing load approach 0 Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼2箇所+ジェット燃焼2箇所として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various energy storage cycles driven by oxygen combined water injection unit (88K) as a vertical type moving blade ratio critical material gravity turbine (8N) power generation electrical product + rocket combustion 2 locations + jet combustion 2 locations with magnetic bearing load approaching 0 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼3箇所+ジェット燃焼3箇所として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various energy storage cycles driven by oxygen combined water injection unit (88K) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 3 rocket combustion + 3 jet combustion Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼4箇所+ジェット燃焼4箇所として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various energy storage cycles driven by oxygen combined water injection unit (88K) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 4 rocket combustion + 4 jet combustion 4 locations with magnetic bearing load approaching 0 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼5箇所+ジェット燃焼5箇所として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycles driven by oxygen combined water injection unit (88K) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 5 rocket combustion + 5 jet combustion 5 locations with magnetic bearing load approaching 0 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼6箇所+ジェット燃焼6箇所として酸素合体水噴射部(88K)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycles driven by oxygen combined water injection unit (88K) as a vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 6 rocket combustion + 6 jet combustion 6 locations with magnetic bearing load approaching 0 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼+ジェット燃焼として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Combined engine and coalescence of various energy storage cycles driven by oxygen coalesced air injection unit (88A) as rocket-type combustion product + rocket combustion + jet combustion Method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼2箇所+ジェット燃焼2箇所として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycles driven by oxygen combined air injection unit (88A) as a vertical type moving blade ratio critical material gravity turbine (8N) generator electric product + 2 rocket combustion + 2 jet combustion 2 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼3箇所+ジェット燃焼3箇所として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycles driven by oxygen combined air injection unit (88A) as a vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 3 rocket combustion + 3 jet combustion Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼4箇所+ジェット燃焼4箇所として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycle driven by oxygen combined air injection unit (88A) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 4 rocket combustion + 4 jet combustion 4 locations with magnetic bearing load approaching 0 Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼5箇所+ジェット燃焼5箇所として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various type of energy storage cycle driven by oxygen combined air injection unit (88A) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 5 rocket combustion + 5 jet combustion Merger engine and merger method. 磁気利用軸受荷重0接近とした竪型全動翼比重大物質重力タービン(8N)発電電気製造物+ロケット燃焼6箇所+ジェット燃焼6箇所として酸素合体空気噴射部(88A)駆動する各種エネルギ保存サイクル合体機関及び合体方法。   Various types of energy storage cycle driven by oxygen combined air injection unit (88A) as vertical type moving blade ratio critical material gravity turbine (8N) power generation electric product + 6 rocket combustion + 6 jet combustion locations Merger engine and merger method.
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