JP2013119790A - Various energy preserving cycle united engine - Google Patents

Various energy preserving cycle united engine Download PDF

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JP2013119790A
JP2013119790A JP2011267437A JP2011267437A JP2013119790A JP 2013119790 A JP2013119790 A JP 2013119790A JP 2011267437 A JP2011267437 A JP 2011267437A JP 2011267437 A JP2011267437 A JP 2011267437A JP 2013119790 A JP2013119790 A JP 2013119790A
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coalescence
combustion
superheated steam
electricity
oxygen
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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 a problem of existing steam turbine power generation in which a steam speed is reduced to 1/10 by damming up the steam speed by having stator blades which are nil in power factor by a half, a maximum speed part is 43,000 times volume of water, and a power generation output is almost zero.SOLUTION: A power generation quantity of 1/10 or smaller by damming up a lightweight steam speed by including the stator blades which are nil in the power factor by a half, and lightweight object power generation is improved to provide an electricity+liquid air+superheated steam hot heat supply facility 3D for generating sunlight heater heat for inexpensive electric driving such as a power generation cost of 1/100 such as a fuel cost 0 by aiming at 0 of a power generation quantity bearing load of existing 1,355 times on a one unit power generation quantity of superposing 100 sets of mercury injection turbines by aiming at Mach 30, for example, as mercury gravity acceleration power generation in 30 mmHg vacuum for doubly reversing the whole moving blades by a horizontal shaft 1h gear, an automobile, a ship, and an aircraft are set in a volume compression power of 21/60,000 of air compression as liquid oxygen compression driving and set in a 1/10 fuel cost and a 10-time speed, the aircraft is aimed at a 1/500,000 space arrival cost so as to enable a day' trip anywhere on the earth, and thus an operational profit for operating the whole manufacturing object becomes preeminently and permanently best in the world.

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本発明液体噴射速度+真空中重力加速度でマッハ30水銀駆動や、超高速円周速度狙う内外夫々円筒軸装置に6種類の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8Q発電は、反発永久磁石9B+吸引永久磁石9Cで軸受荷重0接近+超高速周速度にし、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828mに100組等タービン発電する、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+マッハ3以上高速噴射追加+タービン数無制限落差無制限追加して、例えばマッハ28等狙う水銀噴射真空中重力加速や、落差500〜828mにタービン100組既存揚水発電の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3Q回転力駆動や、酸素合体空気噴射部88Bや酸素合体水噴射部88L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、飛行機や船舶は10倍速度狙い、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 gravity-type gravity turbine with a significant ratio of vertical rotor blades, which is fitted with six types of annular turbine blade groups on both the inner and outer cylindrical shaft devices that drive Mach 30 mercury with liquid jet velocity + gravitational acceleration in vacuum and ultra high speed circumferential speed. 8Q power generation is reversible permanent magnet 9B + attracting permanent magnet 9C to make bearing load close to 0 + super-high speed peripheral speed, and reverse inversion one after the other by the double reversal magnetic device 85 + horizontal axis 1h magnetized on the outer periphery of the gear, and the vibration reduction head 100 sets of turbines are generated in 828m, the largest unutilized renewable energy of the earth is added to the existing pumped-storage power generation, gravity acceleration during vacuum increase + Mach 3 or higher high speed injection added + turbine number unlimited head drop unlimited limit, for example Mach 28 Mercury injection vacuum acceleration in vacuum, aiming for a power generation of 10,000 times the existing pumped-storage power generation of 100 sets of turbines with a drop of 500 to 828 m, various fuel costs of boilers and nuclear reactors abolished As necessary power generation, gravity turbine 8N power generation electric drive 1 to multistage heat pump 1G and solar heater 21 are used, and solar heating air is compressed to high temperature, and heat recovery is divided and stored in 1 to multistage compression heat recovery unit 2C. 24 to 200MPa superheated steam 50 warm heat + liquid air 28a cold heat, divided into electricity + liquid air cold heat + superheated steam heat supply equipment 3D endless application, for example, ships, vehicles and airplanes are liquid oxygen The compression volume work rate is set to 21/60000 volume work rate of air compression, the compression pressure of liquid oxygen or water is made 20 times easier, and the theoretical expansion engine 3Q rotational force drive or oxygen combined air injection unit 88B And oxygen coalescence water injection unit 88L for coalescence injection propulsion, ship coalescence injection propulsion, natural phenomenon speeding up 2a supply nitrogen, oxygen and CO2 to seawater increase microorganisms and seaweed, The human food such as fish is greatly increased, etc., and the driving of airplanes and automobiles aims to reach 1/10 of CO2 exhaust, 1/10 of the fuel cost and 1 / 500,000 cost space, and 10 times the speed of airplanes and ships, and save various energy The present invention relates to a technology of a cycle coalescence engine and various energy storage coalescence methods.

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8Q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を受給して液体酸素5Kの圧縮にし、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+高温水52aを超高圧に圧縮理論燃焼室4Q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4Qに夫々を噴射する過程で燃料噴射燃焼し、超高圧酸素+超高圧燃料高温燃焼で超高圧高温過熱蒸気50を加熱して、超高圧酸素超高圧燃料炎3000℃以上過熱蒸気の熱分解電気分解狙い酸素水素増大燃焼の各種研究にし、理論燃焼室4Q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3Q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、運用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 most existing car-driven reciprocating engine in the world consumes enormous amount of fuel due to air compression, and the vertical type moving blade ratio critical material gravity turbine 8Q vacuum critical 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 under the sea, methane and water are divided into methane and liquid nitrogen cooled liquid methane is recovered and liquid oxygen chamber 5K receives liquid oxygen 5K Then, compression of liquid oxygen 5K, compression volume work rate of 21/60000 volume work of air compression, 24-200MPa ultra-high pressure compression injection, liquid oxygen 5K + liquid fuel 1b + high temperature water 52a compression theory to ultra high pressure Fuel is injected and burned in the process of heating at the inner circumference of the combustion chamber 4Q, etc., and injecting each into the theoretical combustion chamber 4Q by heating to an ultra-high temperature or optimum temperature, ultra-high pressure oxygen + ultra-high pressure The super high pressure high temperature superheated steam 50 is heated in the high temperature combustion of the material, and the super high pressure oxygen super high pressure fuel flame 3000 ° C. or more is used for various researches of the oxygen hydrogen hydrogen combustion for the thermal decomposition electrolysis of the superheated steam. The combustion gas 49 + superheated steam 50 is injected from the high-pressure / high-temperature combustion gas control valve 5a or the combustion gas injection nozzle 6Y to drive the theoretical expansion engine 3Q to drive various vehicles such as automobiles and tillers, propellers 7A and rotor blades 7B. And drive 7C, drive various vehicles, propeller airplanes and screw ships, aim for fuel cost 1/10 or 10 times speed by using liquid oxygen 5K of electricity generation electricity production, excellent operating profit rate world The present invention relates to various energy storage cycle coalescence engines and coalescence techniques.

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周等宇宙飛行が空気圧縮では不可能なため、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88B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8Q発電電気駆動多数の1〜複数段理論気体圧縮機3T等熱ポンプ1G+太陽光加熱器21熱製造により、24〜200MPaの高温水〜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1c+高温水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88B理論燃焼室4Q内周の、燃料加熱管1L水加熱管5H酸素加熱管5Hで加熱最適温度にし、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以上の理論超高圧燃焼狙う理論燃焼室4Qに噴射燃焼し、酸素噴射ノズル6L燃料噴射ノズル6X複数中央燃焼3300℃以上で熱分解電気分解狙いとして、過熱蒸気で酸素水素増大燃焼狙い+ロケット燃焼前方の空気を吸引噴射し、1〜複数段吸引空気流ジェット燃焼追加にして、理論燃焼室4Q過熱蒸気噴射ノズル6A過熱蒸気50を200MPa狙い噴射で、燃焼ガス49を吸引噴射する、ロケット燃焼で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 consumes enormous amount of fuel by air compression, and the rotation output and injection propulsion output are reduced, and space flight such as 16 rounds of the earth on the day of the air resistance 01 is impossible by air compression. As the aim of propulsion of liquid compressed oxygen coalesced air injection unit 88B, which combines the two types, vertical type moving blade ratio critical material gravity turbine 8Q power generation electric drive multiple 1 to multi-stage theoretical gas compressor 3T equal heat pump 1G + solar heater 21 heat production, 24 to 200 MPa high-temperature water to superheated steam temperature 50 + liquid air cold heat 28a is divided and stored. As electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D, the jet propulsion of the aircraft is liquid oxygen 5K + liquid fuel 1c + Received by high-temperature water 52a and compressed by compression of liquid oxygen, compressed volumetric power is compressed by air compression 21/60000 Open the valve 5T + water control valve 5Q + liquid fuel control valve 1K, set the fuel heating pipe 1L water heating pipe 5H oxygen heating pipe 5H to the optimum heating temperature of the oxygen combined air injection part 88B theoretical combustion chamber 4Q, and control the fuel. Open the valve 25b + oxygen control valve 24D + superheated steam control valve 25 and inject each one into the theoretical combustion chamber 4Q aiming at one or more theoretical ultra-high pressure combustion, oxygen injection nozzle 6L fuel injection nozzle 6X multiple central combustion at 3300 ° C. or more As a target for pyrolysis and electrolysis, superheated steam aims to increase oxygen-hydrogen combustion + air in front of rocket combustion is sucked and injected, and 1 to multi-stage suction air flow jet combustion is added, theoretical combustion chamber 4Q superheated steam injection nozzle 6A superheated steam 50 is targeted for 200MPa injection, combustion gas 49 is sucked and injected, and rocket combustion is aimed at the existing space cost of 1 / 500,000. To allow a day trip to one day in a row anywhere on Earth equal to 16 laps of the earth, aiming profit margin 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理論気体圧縮機3T使用追加とし、竪型全動翼比重大物質重力タービン8Q発電電気駆動1〜複数段理論気体圧縮機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高温水52a〜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+高温水52aを受給過程でポンプ圧縮200MPa狙いとし、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88L理論燃焼室4Q内周で夫々最適温度に加熱し、酸素合体水噴射部88Lや理論膨張機関3Qに噴射夫々を水吸引噴射駆動や回転駆動して、酸素合体水噴射部88Lの水吸引噴射推進や理論膨張機関3Q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、スクリュウ推進理論膨張機関3Q排気は船底先頭部排気噴射推進とし、摩擦低減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, liquid air production air compressor is also the best theoretical gas compressor 3T use, vertical full blade ratio material gravity turbine 8Q power generation electric drive 1 to multi-stage theoretical gas compressor As the heat pump 1G compression for 3T, etc., the solar heating device 21 is made into a heat production in which the solar heating air is compressed at a high temperature and the heat recovery is divided and stored in the 1-stage multi-stage compression heat recovery device 2C. Superheated steam 50 heat + liquid air 28a cold storage divided into electricity, liquid air cold heat + superheated steam heat supply equipment 3D, pumping liquid oxygen 5K + liquid fuel 1c + hot water 52a in the process of receiving Aiming at 00 MPa, the liquid oxygen control valve 5T + the liquid fuel control valve 1K + the water control valve 5Q are opened, and the oxygen combined water injection part 88L is heated to the optimum temperature in the inner periphery of the theoretical combustion chamber 4Q, respectively. Each of the injections to the theoretical expansion engine 3Q is driven by water suction injection or rotationally driven to promote water suction / injection propulsion of the oxygen combined water injection unit 88L or to rotate the screw 7C of the theoretical expansion engine 3Q. / 10 As a fuel cost target, the screw propulsion theoretical expansion engine 3Q exhaust will be the bottom bottom exhaust injection propulsion, the natural phenomenon speeded up in the process of friction reduction injection propulsion, supplying oxygen, nitrogen, CO2 etc. into the sea, It is related to the technology of various energy conservation cycle coalescence engines and coalescence methods aiming at the world's highest profit rate by increasing the food of human beings that proliferate phytoplankton, seaweeds, corals, fish, etc. .

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+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. In order to achieve this, a turbine blade that supports 240 times volume from 240 atmospheres to atmospheric pressure +30 times, 4 times Hg, and 25 times capacity, and 6000 times capacity can be used. There is a necessary background, in addition to responding to the turbine blade area, the seawater temperature is raised by 7 degrees with all the generated heat, making the whole sea surface temperature rise impossible natural phenomenon, increasing abnormal weather without upper limit, 50 to 100 years People in heavy rains of seawater before and after There 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例えば水銀仕事率にして、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組で23000倍発電量等膨大な発電量が予想され、更に実験が必要な真空中水銀重力加速度マッハ30狙い燃料費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組組立で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マッハ30狙い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〜複数段理論気体圧縮機3T等熱ポンプ1Gで複数回圧縮複数回熱回収して、24〜200MPa高温水52a〜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 converted into a mercury-accelerated power generation in a vacuum by using 23,000 times more important material than the existing steam turbine power generation. Power generation is 230 times higher than that of the existing steam turbine power generation, but a huge power generation amount of 23,000 times power generation is expected in 100 pairs at a height of 500m or more, and further mercury gravity acceleration Mach 30 in vacuum is necessary for further experiments Infinite power generation with zero fuel cost generation, vertical type full blade ratio material mercury gravity turbine 8N power generation cylinder inner rotor blade group 60C cylindrical outer rotor blade group 60D, fully automatic machining including cylinder assembly fixed rotor blade group, respectively Easy and easy assembly, 1/10 number of parts, etc., 1/10 parts fully automatic machining 100 sets assembly, aiming for 23000 times power generation, mercury gravitational energy in the earth's largest gravity acceleration acceleration in Mach 30 Driven to the expansion of low-cost electricity applications with zero fuel cost power generation by a large amount of mercury resources, solar heating the air with the solar heater 21, mercury gravity turbine 8N fuel cost zero power generation electric drive 1 Multiple-stage theoretical gas compressor 3T, etc. Compressed multiple times with heat pump 1G, recovered heat multiple times, divided and stored in 24-200MPa high temperature water 52a-superheated steam temperature 50 + liquid air cold 28a, electricity + liquid air cold + superheated steam It is supplied from the hot heat supply facility 3D and received by the liquid oxygen chamber 5K, storage battery, etc., and the liquid air driven car, airplane or ship is driven by 1/10 fuel cost or 10 times speed driving to generate extremely inexpensive power. There are backgrounds in which storage battery driving, electric driving, and prevention of global warming with little CO2 exhaust are obtained.

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8Q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〜複数段理論気体圧縮機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+温熱の高温水52a〜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, when the vertical turbine-type critical material gravity turbine 8Q power generation is used, there is a background of low fuel cost power generation, and the case of heating a huge 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 fuel cost 0 power generation electric drive solar heater 21 is used, and the heat pump 1G such as the 1-multistage theoretical gas compressor 3T or the 1-multiple stage compression of the air 28a heated by sunlight with the fuel cost 0 power generation electric drive is used. In the heat recovery unit 2C, the heat is recovered multiple times and heat is recovered multiple times, divided into 5K cold liquid oxygen and 5L liquid nitrogen + hot high temperature water 52a to superheated steam 50, and in the process of infinite use of heat, for example permafrost Injecting superheated steam 50 into underground methane hydrate, splitting it into methane and water, recovering methane with liquid nitrogen cooled liquid methane and continuing the superheated steam injection forever, the methane recovery enclosure has a suitable temperature and lots of water droplets Land grazing, increasing the use of food by humans, and infinite use of heat, aiming to reach 1 / 500,000 in space-driven costs for liquid air-powered cars, ships and spacecrafts, and speeding natural phenomena in the process of ship driving 2a , Fine And the seaweed and coral, 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2011−247103号出願日平成23年9月30日まで19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 19 applications, including PCT, from the filing date of Japanese Patent Application No. 2011-247103 to September 30, 2011.

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財政黒字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 the invention that keeps 100% monopoly on the world scale forever, there is a challenge to make the world's most eternal financial surplus with outstanding profitability forever.

竪型全動翼比重大物質重力タービン8Q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〜複数段理論気体圧縮機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+高温水〜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4Qとして、酸素燃料超高圧燃焼複数中心付近燃焼で高圧高温過熱蒸気50を加熱し、酸素燃料超高圧燃焼炎3000℃以上燃焼で過熱蒸気の熱分解電気分解狙い酸素水素増大燃焼狙いにして、理論燃焼室4Q駆動の理論膨張機関3Qや酸素合体水噴射部88Lや酸素合体空気噴射部88B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や自動車等として、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。 Vertically moving blade ratio critical material gravity turbine 8Q fuel cost 0 power generation cheap electric drive all, heat production by solar heater 21 + 1-multistage theoretical gas compressor 3T etc. heat pump 1G + 1-multistage compression heat recovery unit 2C Then, as electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply facility 3D, the received liquid oxygen 5K is compressed to 21/60000 volumetric compression work rate of air compression, and super high pressure combustion and super high temperature combustion are easy As the theoretical combustion chamber 4Q, high-pressure high-temperature superheated steam 50 is heated by near-center combustion of oxyfuel ultra-high pressure combustion, and thermal decomposition electrolysis of superheated steam is aimed at combustion of 3000 ° C or more of oxyfuel superheated steam, aiming at increased oxygen-hydrogen combustion Thus, a theoretical expansion engine 3Q driven by a theoretical combustion chamber 4Q, an oxygen combined water injection unit 88L, and an oxygen combined air injection unit 88B are used to drive or jet vehicles such as automobiles, ships and airplanes. Propulsion drive, ship jet propulsion drive speeds up natural phenomena 2a, supplies oxygen, nitrogen, CO2 etc. into the sea, increases microorganisms, phytoplankton, seaweeds, corals, fish, etc., increases human food The plane is going around the earth 16 times a day in the prime of space flight close to CO2 exhaust 0, etc. Every day on the earth, it is assumed that CO2 exhaust is a little flight anywhere in the atmosphere, 100% global scale monopoly and top secret manufacturing operation As the world's most profitable power generation, ships, airplanes, automobiles, etc., the world's number one with outstanding profitability and the world's largest number of new jobs, preventing droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and earthquakes and tsunamis Prevent global warming and postpone human extinction.

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組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組分全自動製造で100組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と同真空度駆動の横型全動翼水重力タービン8N発電を、最大速度の最終動翼群と同真空水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、1/100容積水発電で430倍発電量になります。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8P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組重ねた1台で43000倍発電量を算出に加えて、水噴射速度マッハ3×真空中重力加速度=マッハ30狙いで30倍発電量狙い、更に水銀噴射で406倍発電量が狙える等、実験が必要ですが発電原価を1/10等に大改革して電気製造物雇用無限増大にする効果がある。 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 sets, etc. is very large, all the 100 sets of theoretical best turbine blades 8c of the cylindrical blade group 60C60D The 100-manufacturing effect of automatic production is very large, and the effect of simplifying the structure without the need of a boiler or nuclear reactor is very large. When the turbine 8N power generation is compared with the maximum speed final blade group by the same vacuum water drive, water vapor of 1,700 times volume of water at an atmospheric pressure of 100 ° C. and 760 mmHg is obtained according to Boyle's law at an exhaust temperature of 29 ° C. and a vacuum degree of 30 mmHg. 760mmHg × 1700 = 30mmHg × V2 volume water vapor, V2 = 760/30 × 1700 = water 43,000 times water vapor, 1/100 volume water power generation It will be 430 times the amount of power generation. In other words, vertical all-blade water gravity turbine 8P power generation, which is a group of existing steam turbine maximum speed power blades, is much more advantageous at the power generation stage, and 430 times power generation at 1/100 volume water speed of superheated steam. In addition to increasing the amount, the degree of vacuum increase is far superior, and the use of gravitational acceleration in the vacuum is further increased to 43,000 times the power generation amount calculated by one set of 100 pairs, water injection speed Mach 3 × in vacuum Gravity acceleration = Mach 30 aiming for 30 times power generation target, and mercury injection aiming for 406 times power generation target, but experiments are necessary, but the power generation cost will be greatly reduced to 1/10 etc. to increase the employment of electrical products infinitely effective.

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+高温水〜過熱蒸気温熱供給設備3Dより液体酸素5K等を受給して、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4Q中心付近超高圧高温燃焼で超高圧過熱蒸気50の増大+熱分解電気分解狙いとして、理論燃焼室4Qにより理論膨張機関3Qや酸素合体水噴射部88Lや酸素合体空気噴射部88B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3Q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 + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen 5K, etc., and the compression work rate of combustion oxygen is 21/60000 volumetric compression work of air compression The theoretical combustion chamber 4Q uses the theoretical expansion engine 3Q, the oxygen coalescence water injection unit 88L, and the oxygen coalescence air injection as an aim to increase the superhigh pressure superheated steam 50 in the superficial combustion chamber 4Q center and increase the pyrolysis electrolysis. Part 88B has the effect of being able to drive the most efficiently, and in addition to the effect of targeting 1/10 or 10 times the fuel cost of automobiles, ships and airplanes, the space arrival cost is aimed at 1 / 500,000 of existing space rockets The wheel, screw 7C, propeller 7A and rotor blade 7B are driven by the theoretical expansion engine 3Q, and the ship, airplane, car, etc. are driven by the rotational force, and the ship injection propulsion drive is used. Natural phenomenon speeding up 2a, and the effect of increasing the digestive capacity of underwater microorganisms such as CO2 to tens of thousands of times of the forest, etc. is great, and phytoplankton, seaweeds, corals, etc. are propagated, and fish and other human beings in the food chain etc. Greatly increase undersea food, prevent desertification, droughts, torrential rains, typhoons, seasonal winds, earthquake tsunamis, etc., postpone the most important human extinction of humanity, and aim to achieve the world's best profit rate is there.

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8Q発電電気駆動の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備より液体酸素高温水を受給し、液体酸素5K+液体燃料1c+高温水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を開放し、理論燃焼室4Q内周の燃料加熱管1L+酸素加熱管5F+高温水加熱管5Hを最適過熱して、燃料制御弁25b酸素制御弁24Dを開放し、酸素ガス+燃料ガス複数個所中心付近混合噴射着火燃焼して、理論燃焼室4Q内周の燃料加熱管1L+酸素加熱管5F+高温水加熱管5Hを最適過熱し、超高圧高温過熱蒸気50等に過熱して、最高温度超高圧燃焼で理論燃焼室4Q過熱蒸気熱分解電気分解狙い酸素水素増大燃焼狙いにし、酸素合体空気噴射部88B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、24〜200MPa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 high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment of fuel cost 0 type all blades important material gravity turbine 8Q power generation electric drive, liquid oxygen 5K + liquid The fuel 1c + high temperature water 52a is compressed by ultra high pressure with the liquid fuel pump 4a + liquid oxygen pump 4b + water pump 4c, the liquid fuel control valve 1K + liquid oxygen control valve 5T + water control valve 5Q is opened, and the inside of the theoretical combustion chamber 4Q is The fuel heating pipe 1L + oxygen heating pipe 5F + high temperature water heating pipe 5H is optimally heated, the fuel control valve 25b and the oxygen control valve 24D are opened, and the mixed injection ignition combustion is performed in the vicinity of the center of the oxygen gas + fuel gas plural places, the theoretical combustion chamber 4Q inner circumference fuel heating pipe 1L + oxygen heating pipe 5F + high temperature water heating pipe 5H is optimally heated, superheated to super high pressure high temperature superheated steam 50, etc., and theoretical combustion chamber 4Q superheated steam with maximum temperature super high pressure combustion Aiming at pyrolytic electrolysis aiming at increased oxygen hydrogen combustion, driving the oxygen coalesced air injection unit 88B, aiming for space arrival cost 1 / 500,000 of existing space rocket, using the same fuel cost 10 times injection propulsion output It has the effect of aiming for prime, for example, the jet propulsion output is aimed at 100 times the pressure of existing jets, 10 times the calorie injection, and 1000 times the propulsion output for the short time. Since the steam injection speed and the combustion gas injection speed are the highest in vacuum, the existing space rocket ground mass injection is considered the worst, and from the vicinity of the highest flight altitude of the existing aircraft, high pressure high temperature combustion gas 5M + 5N high pressure high temperature steam 5N There is an effect that the injection amount is increased and the earth is made 16 times a day, etc., and the space use prime that allows a day trip anywhere on the earth can be aimed.

竪型全動翼比重大物質重力タービン8Qの1h9C9Bの説明図(実施例1)Explanatory drawing of 1h9C9B of vertical type moving blade ratio critical material gravity turbine 8Q (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3Qの5b6X6Y9B9C9D9E5の説明図(実施例5)Explanatory drawing of 5b6X6Y9B9C9D9E5 of theoretical expansion engine 3Q (Example 5) 酸素合体水噴射部88Lの説明図(実施例6)Explanatory drawing of oxygen combined water injection part 88L (Example 6) 酸素合体空気噴射部88Bの説明図(実施例7)Explanatory drawing of the oxygen coalescence air injection part 88B (Example 7) 理論膨張機関自動車4Lの説明図(実施例8)Explanatory drawing of the theoretical expansion locomotive 4L (Example 8) 酸素合体スクリュー船舶39Qの説明図(実施例9)Explanatory drawing of oxygen coalescence screw ship 39Q (Example 9) 酸素合体スクリュー噴射船舶39Sの説明図(実施例10)Explanatory drawing of the oxygen coalescence screw injection ship 39S (Example 10) 酸素合体噴射船舶39Rの説明図(実施例11)Explanatory drawing of oxygen coalescence injection ship 39R (Example 11) 酸素合体噴射飛行機39Tの説明図(実施例12)Explanatory drawing of the oxygen coalescence injection plane 39T (Example 12) 酸素合体プロペラ飛行機39Uの説明図(実施例13)Explanatory drawing of oxygen combined propeller plane 39U (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組重ねた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8Q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 vacuum for a long period of time is prevented by brainwashing such as existing steam turbine power generation, and one unit of 100 sets 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 Except for the specific material gravity turbine 8Q, we will explain in substitution for three examples, and try to materialize the invention without common sense.

図1真空中重力加速度+水銀噴射速度でマッハ30駆動等極限狙う、竪型全動翼比重大物質重力タービン8Q発電は、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で水銀3Eで2E混合噴射真空中重力加速度加速マッハ30狙いの駆動にし、円筒内側動翼群60C円筒外側動翼群60D超高速タービン周速度記録更新狙いにして、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8Q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、動翼群を円筒環状組立9Aに嵌合構成して、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夫々図2の6部品を、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8Q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 Gravity acceleration in vacuum + mercury injection speed, Mach 30 drive, etc., aiming to the limit, vertical type moving blade ratio critical material gravity turbine 8Q power generation is proportional to kg weight m / sec. Each shaft device 60B is provided with a repulsive permanent magnet 9B attracting permanent magnet 9C, each bearing is made close to the bearing load by the repulsive force or attracting force, and there are a plurality of ring-type double-sided two-pole magnetisms, so Aiming at an infinite increase in diameter, the specific critical material 2E3E is raised by 500 to 828 m, etc. by the specific critical material raising device 2F, and the specific critical material accelerator 6W is driven by mercury 3E and 2E mixed injection vacuum gravity acceleration acceleration Mach 30 target driving The cylinder inner rotor blade group 60C and the cylinder outer rotor blade group 60D are super-high speed turbine peripheral speed record renewal target, and the vertical type whole blade ratio critical material gravity turret driven 100 pairs etc. one after the other with the horizontal axis 1h gear. 8Q power generation, the inner shaft device 60A and the outer shaft device 60B are each provided with a cylindrical portion to facilitate full automatic processing and assembly, and the moving blade group is fitted to the cylindrical annular assembly 9A. In the manufacturing process, the cylinder inner rotor blade group 60C and the cylinder outer rotor blade group 60D are each made up of six components as shown in FIG. Are fixed to 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. The six parts are fully automatic casting, fully automatic processing, cemented carbide surface treatment, etc. Gravity acceleration for vacuum acceleration of water as a thrust bearing 80a and bearing 80 including permanent magnets and electromagnets that support weight, making mass production inexpensive and easy to manufacture, such as cylindrical annular assembly 9A, etc. 1g, and the gravity acceleration part 1g joint has a horizontal shaft 1h through hole for driving the generator 1, and the generator 1 is driven plurally outside the turbine outer box 77a, so that the multistage saddle type all blade specific gravity Large material gravity turbine 8Q Rotation direction alternate drive, the next turbine 8N is driven one after another by acceleration of gravity acceleration part 1g, and the horizontal axis 1h is alternately driven to make the electric product infinity and electric drive infinity with simple structure, The world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profitability.

竪型全動翼比重大物質重力タービン8Q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、内側軸装置60Aや外側軸装置60Bの推力軸受80aは磁気利用軸受荷重0狙いとして、軸受80具備して横軸1h歯車で二重反転磁気装置85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による噴射速度+真空中の重力加速度=マッハ30狙い噴射速度として、例えば水銀3E圧力で白金球2E混合噴射とし、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30狙い速度を維持して、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8Q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と比較では、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8Qマッハ1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 8Q power generation consists of 6 parts in one set with two kinds 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 bearings 80a of the inner shaft device 60A and the outer shaft device 60B are provided with bearings 80 to form a counter rotating magnetic device 85 with a horizontal shaft 1h gear, and a cylindrical inner rotor blade group. The 60C cylindrical outer rotor blade group 60D is driven by a double reversal drive that rotates alternately for each turbine, and the vibration and noise are reduced by the turbine drive that cancels the resonance. The injection speed by the specific material accelerator 6W + the gravitational acceleration in the vacuum = Mach As a target jet speed, for example, platinum ball 2E mixed injection is performed with mercury 3E pressure, and as the acceleration effect of gravitational acceleration in vacuum is the highest, the cylinder inner rotor blade group 60C is injected into the cylinder outer rotor blade group 60D, respectively. The horizontal axis 1h counter-rotating drive power generation to maintain the target speed of Mach 30 and drive the next turbine to make a vertical full blade ratio critical material gravity turbine 8Q power generation that effectively uses the head, and frictional heat cooling In the air extractor 51, the existing power generation maximum vacuum degree, such as 30 mmHg, is easily used, and 100 to 200 sets are used for the drop 828 m. Compared with the final stage of the existing steam turbine power generation, the water degree is 43,000 times the Mach 1 speed water vapor of 30 mmHg water. In comparison with one turbine 8Q Mach 1 power generation in which 100 sets are stacked, 1/1000 volume of mercury is 43 × 100 × 13, 55 = 58265 times the amount of mercury power generation by Mach 1 speed injection, and 91891 for platinum balls Energy saving cycle coalescence engine fuel cost becomes extremely low 0 To power.

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、図1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、燃料費0等比較物皆無の運用利益率抜群世界一にする、竪型全動翼比重大物質重力タービン8Q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 in FIG. 1 are each provided with a cylindrical annular assembly 9A, and the outer shaft device 60B and the cylindrical annular assembly 9A are fixed to the inlet fixed outer blade 60E in an annular fitting assembly. The inlet rotor blade group of the cylindrical outer rotor blade group 60D is constituted, and the inner shaft device 60A and the cylindrical annular assembly 9A are fixed to the inlet fixed inner blade 60F, and the inlet rotor blade group of the cylindrical inner rotor blade group 60C is fixed. The outer shaft device 60B and the cylindrical annular assembly 9A are configured by an 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 disposed on the inner side. With annular wing 60H annular fitting assembly, The intermediate rotor blade group of the cylinder inner rotor blade group 60C is constituted, and the outer shaft device 60B and the cylindrical annular assembly 9A are annularly fitted to the outer annular blade 60G, and the second intermediate rotor blade group of the cylindrical outer rotor blade group 60D. The inner shaft device 60A and the cylindrical annular assembly 9A are configured by fixing the outlet fixed inner blade 60K in an annular fitting assembly to form the 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 annularly assembled and fixed to form the outer rotor blade group of the cylindrical outer blade group 60D, and each of the six types of cylindrical rotor blade groups 60 is manufactured by fully automatic processing, etc. As a result, the manufacturing cost is extremely low due to the simplicity of the structure, no boilers, no reactors, etc., making it the world's best operating profit rate with no comparison of fuel costs, etc. 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8Q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等を熱ポンプ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24〜200MPa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 8Q fuel cost 0 power generation Extremely inexpensive electric drive, inexpensive 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. Intake and compression as 1 to multiple stage heat pump 1G for suction, theoretical gas compressor 3T and the like as heat pump 1G are set to 800 to 1200 ° C multiple times, and heat recovery is repeatedly performed at 1 to multiple stage compression heat recovery unit 2C. Then, the liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L, and the 24-heat of about 200-400 MPa superheated steam 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安価増大狙う、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8Q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等の熱ポンプ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+高温水〜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, ultra-high speed rotation, and compression ratio greatly increased, and uses magnetic force + air pressure. With a bearing load approaching zero or using heat of vaporization, the compression ratio of one unit is greatly increased, and Boyle's law gas volume is inversely proportional to the pressure. The best aim is to compress the suction from the large circumferential blade to the central short blade. As a result, the maximum intake air amount is aimed at, and the intake air velocity is aimed at the maximum at the upper compression blade group 8g and the lower compression blade group 8h of all the rotor blades, and the assembly compression blade group 8j facilitates assembly and suction. Mouth area maximum ease and compression efficiency best aiming, vertical type moving blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extremely cheap electric drive, double reversal magnetic (gear) device 85 (85Y) of horizontal axis 1h gear The upper compression blade group 8g The side compression blade group 8h is rotated in the opposite direction to rotate in the opposite direction, the relative peripheral speed is 3 to 10 times that of the existing axial flow compressor, the theoretical gas compressor 3T is the best theoretical gas compressor 3T, and the final compression blade 6 stationary blade 6G The heat production is to press fit into the compressed air heat exchanger 2Y, and the heating air of the solar heater 2 is mainly compressed with a heat pump 1G such as the theoretical gas compressor 3T, and 1 to a plurality of stages of compression heat for each compression high temperature. Heat is recovered by the recovery unit 2C, divided and stored as liquid air cold heat + superheated steam temperature heat, and used as a supply facility 3D for electricity + liquid air cold heat + hot water to superheated steam temperature heat. For use in infinite heating applications such as greenhouse cultivation, inexpensive liquid oxygen is used for driving automobiles, ships and airplanes with a compression work rate of 21/60000 of air compression, and inexpensive liquid nitrogen is used for infinite use for cooling such as ice production, Various uses You use.

図5の超高圧極限燃焼で酸素水素増大燃焼狙う理論膨張機関3Q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8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、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+高温水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を開放し、理論燃焼室4Q内壁燃料加熱管1L高温水加熱管5H酸素加熱管5Fで最適温度に加熱して、図に無い上流過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放し、超高圧燃料酸素中心付近複数3000℃以上燃焼して、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200MPa狙い過熱蒸気50を過熱蒸気噴射ノズル6A噴射して、燃焼ガス噴射ノズル6Y燃焼ガス49を吸引噴射し、圧縮吸入空気路5b空気噴射ノズル5の圧縮空気部9D空気を吸引噴射して、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、燃料燃焼量を増大する理論膨張機関3Q駆動にして、燃焼ガス49を高圧高温燃焼ガス49とし、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3Q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3Qとする。 The theoretical expansion engine 3Q aiming at oxygen-hydrogen increase combustion in the ultra-high pressure extreme combustion of FIG. 5 is equipped with 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. From the use of electricity + liquid air cold heat + hot water to superheated steam hot water supply equipment 3D, which uses magnetic force + air pressure to make the bearing load close to 0, and the vertical blade dynamic material gravity turbine 8Q fuel cost 0 power generation extremely cheap electricity production By receiving liquid oxygen 5K + electricity + high temperature water 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 + high temperature water 52a is 24 Compressed to ultra-high pressure such as ~ 200 MPa, liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, theoretical combustion chamber 4Q inner wall fuel heating pipe 1L high temperature water heating pipe 5H oxygen heating pipe 5 Then, the upstream superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b (not shown) is opened and burned at 3000 ° C. or more in the vicinity of the super high pressure fuel oxygen center, and a part of the superheated steam 50 is burned. Aspirating pyrolysis electrolysis oxygen oxygen hydrogen increase combustion aiming near the center, 200MPa aiming superheated steam 50 heated to the optimum temperature on the inner wall is injected with superheated steam injection nozzle 6A, combustion gas injection nozzle 6Y combustion gas 49 is sucked and injected, Compressed intake air passage 5b The compressed air portion 9D of the air injection nozzle 5 is sucked and injected, and the theoretical expansion engine 3Q is driven to increase the fuel combustion amount significantly by increasing the fuel injection combustion combustion amount from the fuel injection nozzle 6X of the fuel pipe 25c. Then, the combustion gas 49 is changed to a high-pressure high-temperature combustion gas 49 and injected from the center in a circumferential direction of 380 degrees, and the upper expansion blade group 8d and the lower expansion blade group 8e are optimally injected. A double inversion driving, the volume of Boyle's law gas as the best theoretical expansion engine 3Q theory which is inversely proportional to the pressure, the theoretical expansion engine 3Q which injects the turbine outer casing 77a assembled turbine blade group 8f.

図6の超高圧極限燃焼で酸素水素増大燃焼狙う、酸素合体水噴射部88L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8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、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+高温水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を開放し、理論燃焼室4Q内壁燃料加熱管1L+高温水加熱管5H+酸素加熱管5Fで最適温度に加熱して、過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放し、超高圧燃料酸素中心付近3000℃以上複数燃焼で高圧高温過熱蒸気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、内壁の保護200MPa狙い過熱蒸気噴射ノズル6A噴射で燃焼ガス49吸引噴射する、超高圧高温ロケット燃焼噴射にして、空気吸引流に燃料噴射ノズル6X複数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、最も超高圧が容易な過熱蒸気50を中核過熱噴射で最大噴射速度とし、前方の空気28aを吸引噴射して前方の水52aを吸引噴射して、酸素合体水噴射部88L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 coalescence water injection unit 88L aiming at oxygen-hydrogen increase combustion in the ultra-high pressure extreme combustion of FIG. 6 is a vertical all-blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extremely cheap electricity production By receiving liquid oxygen 5K + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 of air compression. The volumetric compression work rate is set, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to an ultrahigh pressure such as 24-200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, and the inner wall of the theoretical combustion chamber 4Q The fuel heating pipe 1L + the high temperature water heating pipe 5H + the oxygen heating pipe 5F is heated to the optimum temperature, the superheated steam control valve 25 + the oxygen control valve 24D + the fuel control valve 25b is opened, and the super high pressure fuel acid The high-pressure high-temperature superheated steam 50 is heated by multiple combustion at 3000 ° C. or more in the vicinity of the center, and a part of the superheated steam 50 is aimed at the combustion by suction pyrolysis electrolysis oxygen oxygen hydrogen increase near the center, and the superheated steam injection nozzle 6A aimed at the inner wall protection 200 MPa. Injecting combustion gas 49 by suction, ultra high pressure high temperature rocket combustion injection, fuel injection nozzle 6X multiple fuel injection jet combustion in air suction flow, ultra high pressure high temperature rocket combustion + jet combustion 1 to multiple times, the highest ultra high pressure Various energy storage cycle coalescence engines that make superheated steam 50 easy to achieve the maximum injection speed by core superheat injection, suck air in front of air 28a and suck water in front of water 52a into oxygen combined water injection unit 88L And a coalescence method.

図7の超高圧極限燃焼で酸素水素増大燃焼狙う、酸素合体空気噴射部88B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8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、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+高温水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を開放し、理論燃焼室4Q内壁燃料加熱管1L+高温水加熱管5H+酸素加熱管5Fで最適温度に加熱して、過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放し、超高圧燃料酸素中心付近3000℃以上複数燃焼で高圧高温過熱蒸気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、内壁の保護200MPa狙い過熱蒸気噴射ノズル6A噴射で燃焼ガス49吸引噴射する、超高圧高温ロケット燃焼噴射にして、空気吸引流に燃料噴射ノズル6X複数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、最も超高圧が容易な過熱蒸気50を中核過熱噴射で最大噴射速度とし、前方の空気28aを吸引噴射して酸素合体空気噴射部88B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 unit 88B aiming at oxygen-hydrogen increase combustion in the ultra-high pressure extreme combustion of FIG. 7 is a vertical all-blade ratio significant material gravity turbine 8Q fuel cost 0 power generation extremely cheap electricity production By receiving liquid oxygen 5K + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 of air compression. The volumetric compression work rate is set, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to an ultrahigh pressure such as 24-200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, and the inner wall of the theoretical combustion chamber 4Q The fuel heating pipe 1L + the high-temperature water heating pipe 5H + the oxygen heating pipe 5F is heated to the optimum temperature, the superheated steam control valve 25 + the oxygen control valve 24D + the fuel control valve 25b is opened, and the ultra-high pressure fuel High-temperature high-temperature superheated steam 50 is heated by multiple combustion at 3000 ° C. or more in the vicinity of the elementary center, and a part of the superheated steam 50 is aimed at the combustion by suction pyrolysis electrolytic oxygen hydrogen hydrogen increase near the center, and the superheated steam injection nozzle aimed at the inner wall protection 200 MPa Combustion gas 49 suction injection with 6A injection, ultra high pressure high temperature rocket combustion injection, fuel injection nozzle 6X multiple fuel injection jet combustion in air suction flow, ultra high pressure high temperature rocket combustion + jet combustion 1 to multiple times, the most Various energy storage cycle coalescence engines and coalescence methods are adopted in which superheated steam 50 that is easy to be high pressure is set to the maximum injection speed by core superheat injection, and the air 28a in front is sucked and injected into the oxygen coalescence air injection unit 88B.

図8の超高圧極限燃焼で水素+酸素増大燃焼狙う、理論膨張機関自動車4Lの理論燃焼室4Q理論膨張機関3Q駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、高温水52aを水ポンプ4cで200MPa等に圧縮、液体燃料1cを液体燃料ポンプ4aで圧縮、液体酸素5Kを液体酸素ポンプ4bで圧縮することで、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をを理論燃焼室4Q内壁に供給過熱して、水制御弁5Q開放高温水52aを理論燃焼室4Q内壁に供給過熱し、液体燃料制御弁1K開放液体燃料1cを理論燃焼室4Q内壁に供給過熱して、超高圧最適温度に過熱+200MPa高温過熱蒸気50製造し、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、酸素燃料超高圧中心付近燃焼3000℃以上複数の燃焼にし、内周高温水加熱管5H等を加熱して、過熱蒸気50の一部を中心付近燃焼部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4Q内壁の液体酸素5K+液体燃料1c+高温水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、図に無い高圧高温燃焼ガス制御弁5aを開放理論膨張機関3Q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、理論膨張機関自動車4L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 theoretical combustion chamber 4Q theoretical expansion engine 3Q drive of the theoretical expansion engine automobile 4L aiming at increased combustion of hydrogen + oxygen in the ultra high pressure limit combustion of FIG. 8 is a vertical type full blade ratio material gravity turbine 8Q fuel cost 0 power generation extremely cheap Receives liquid oxygen 5K + electricity + high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, and compresses the high temperature water 52a to 200MPa etc. with the water pump 4c, and the liquid fuel 1c. By compressing with the liquid fuel pump 4a and compressing the liquid oxygen 5K with the liquid oxygen pump 4b, the compression volume work is made 21/60000 volume compression work of air compression, and the liquid oxygen control valve 5T is opened with the liquid oxygen 5K Supply overheat to the inner wall of the theoretical combustion chamber 4Q, supply and overheat the water control valve 5Q open high temperature water 52a to the inner wall of the theoretical combustion chamber 4Q, and supply the liquid fuel control valve 1K open liquid fuel 1c to the inner wall of the theoretical combustion chamber 4Q Supply superheated, superheated to super high pressure optimum temperature + 200MPa high temperature superheated steam 50 manufactured, superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b opened, combustion near oxyfuel super high pressure center 3000 ° C or more The inner peripheral high-temperature water heating pipe 5H and the like are heated, and a part of the superheated steam 50 is aimed at the combustion in the vicinity of the center by the suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion, and the liquid oxygen 5K + liquid fuel on the inner wall of the theoretical combustion chamber 4Q 1c + high temperature water 52a is heated to produce superheated steam 50, fuel, oxygen, inner wall protection combustion or super high pressure / high temperature combustion at the optimum temperature, and open the high pressure / high temperature combustion gas control valve 5a (not shown) to drive the theoretical expansion engine 3Q. Then, the generator 1 is driven to store in the storage battery 1A, the storage battery driving wheel 4J is driven, and the CO2 exhaust 1/10 fuel cost 1/10 operating profit ratio is aimed at 10 times that of the existing automobile. To car 4L, to various energy saving cycle combined institutions and coalescence method.

図9酸素合体スクリュー船舶39Qの超高圧極限燃焼で酸素水素増大燃焼狙う、理論燃焼室4Qの理論膨張機関3Q駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、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+高温水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4Q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を開放して、超高圧燃料酸素中心付近複数3000℃以上の燃焼にし、過熱蒸気50の一部を中心付近燃焼に吸引して、熱分解電気分解酸素水素増大燃焼狙いにし、理論燃焼室4Q内壁の液体酸素5K+液体燃料1c+高温水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3Q1〜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ー船舶39Q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、酸素合体スクリュー船舶39Q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。 Figure 9 The theoretical expansion engine 3Q drive of the theoretical combustion chamber 4Q, aiming to increase oxygen hydrogen in the ultra-high pressure extreme combustion of the oxygen combined screw ship 39Q, is a vertical all-blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extremely cheap electricity By supplying liquid oxygen 5K + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D of manufacturing, and compressing the liquid oxygen 5K into liquid, the compression volume work rate is reduced by air compression. 21/60000 volumetric compression power, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to ultra high pressure such as 24-200 MPa by liquid fuel pump 4a + liquid oxygen pump 4b + water pump 4c, and liquid oxygen control valve 5T + liquid The 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 4Q, the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b Open and burn at a temperature of 3000 ° C. or more near the super-high pressure fuel oxygen center, suck a part of superheated steam 50 into the near-center combustion, aim at pyrolytic electrolysis oxygen-hydrogen increase combustion, Liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is heated to produce superheated steam 50, fuel, oxygen, inner wall protection combustion or super high pressure / high temperature combustion at optimum temperature, and high pressure / high temperature combustion gas control valve 5a is opened. Multiple drive options, screw drive and oxygen coalescence screw ship 39Q to drive, CO2 exhaust 1/10 fuel cost 1/10 operating profit rate 10 times that of existing ship, oxygen coalescence screw ship 39Q, various energy Use a storage cycle coalescence engine and coalescence method.

図10酸素合体スクリュー噴射船舶39Sの超高圧極限燃焼で酸素水素増大燃焼狙う、理論燃焼室4Qによる酸素合体水噴射部88L+理論膨張機関3Q駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、理論膨張機関3Q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88Lに図5理論燃焼室4Qを図6のように移動して、空気28a入口を吸入空気路5bと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4Q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、図6の流線型理論燃焼室4Q1〜複数を用途に合わせて最適具備して、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、200MPa狙い過熱蒸気噴射ノズル6A噴射で燃焼ガス吸引ロケット噴射して、燃料噴射ノズル6X複数ジェット燃焼して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88L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88L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 water injection unit 88L + theoretical expansion engine 3Q driven by the theoretical combustion chamber 4Q, aiming at increased oxygen hydrogen combustion in the ultra high pressure limit combustion of the oxygen combined screw injection ship 39S, is a vertical full blade ratio material gravity turbine 8Q fuel Cost 0 Power generation Extremely inexpensive electricity production of electricity + liquid air cold heat + high temperature water to superheated steam temperature supply facility 3D receives liquid oxygen 5K + electricity + high temperature water, and the screw drive by the theoretical expansion engine 3Q is horizontal in FIG. The shaft 1h drive and the drive similar to the explanation in FIG. 9 are performed, the theoretical combustion chamber 4Q in FIG. 5 is moved to the oxygen coalescence water injection portion 88L as shown in FIG. 6, and the intake air passage 5b is made as close to a straight line as possible. Provided as an injection propulsion, and equipped with a suction air passage 5b around the leading theoretical combustion chamber 4Q combustion gas injection nozzle 6Y, and jet injection is added to the bottom of the jet combustion additional ship for rocket combustion, Six streamlined theoretical combustion chambers 4Q1 to 4Q1 are optimally adapted to the application, liquid oxygen 5K compression is set to 21/60000 volumetric compression work rate of air volumetric compression work rate, and combustion gas is obtained by superheated steam injection nozzle 6A injection targeting 200 MPa. Suction rocket injection, fuel injection nozzle 6X multiple jet combustion, sucking and injecting air in front, sucking and injecting water to make large and small ships, high speed ships and ultra high speed ships to be propelled, for rocket combustion Jet combustion added to increase combustion amount, oxygen combined water injection part 88L 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 Oxygen coalescence water injection unit 88L aiming at 10 times the operating profit rate of existing ships, and various energy conservation cycle coalescence engines and coalescence methods.

図11酸素合体噴射船舶39Rの超高圧極限燃焼で酸素水素増大燃焼狙う、理論燃焼室4Qによる酸素合体水噴射部88L駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、酸素合体水噴射部88Lに理論燃焼室4Qを図6説明のように具備し、先頭理論燃焼室4Q周囲の空気28aを吸入空気路5bとして、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、ロケット燃焼+ジェット燃焼にする、図6流線型理論燃焼室4Q1〜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狙い過熱蒸気噴射ノズル6A噴射で、内部燃焼ガス吸引噴射+ジェット燃焼+前方の空気を吸引噴射+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、酸素合体噴射船舶39R噴射推進空気浮上用の垂直平行板9Qを幅広具備し、空気浮上量最大+摩擦低減量最大として、酸素合体水噴射部88L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88L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 Oxygen hydrogen injection by the theoretical combustion chamber 4Q, aiming at increased oxygen and hydrogen combustion in the ultra-high pressure extreme combustion of the oxygen combined injection ship 39R, is driven by the vertical all-blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extreme Liquid oxygen 5K + electricity + high temperature water is received from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D manufactured by low-cost electric manufacturing, and the theoretical combustion chamber 4Q is shown in FIG. 6 is a streamlined theoretical combustion chamber in which the air 28a around the leading theoretical combustion chamber 4Q is used as the intake air passage 5b, and the fuel injection nozzle 6X injects and burns fuel into the intake air and the like to form rocket combustion + jet combustion. 4Q1-multiple selection according to the application, liquid oxygen 5K compression to 21/60000 volumetric compression work rate of air volumetric compression work, superheated steam injection nozzle aiming at 200MPa With A injection, internal combustion gas suction injection + jet combustion + forward air suction injection + forward water suction injection to make large and small ships, high-speed ships and ultra-high-speed ships to be propelled, jet for rocket combustion Combustion added to increase the combustion amount, the oxygen coalescence injection ship 39R injection propulsion air floating vertical parallel plate 9Q is wide, the air floating amount maximum + friction reduction amount maximum, oxygen combined water injection unit 88L ultra high pressure mass combustion The target is 100 times output, the target is 10 times the speed of the existing ship, the same speed CO2 exhaust 1/10 fuel cost 1/10 the operating profit ratio is 10 times that of the existing ship, oxygen combined water injection unit 88L Energy conservation cycle coalescence engine and coalescence method.

図12酸素合体噴射飛行機39Tの超高圧極限燃焼で酸素水素増大燃焼狙う、理論燃焼室4Qによる酸素合体空気噴射部88B駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、酸素合体空気噴射部88Bに理論燃焼室4Qを図7のように具備し、先頭理論燃焼室4Q周囲の空気28aを吸入空気路5bとして、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、ロケット燃焼+ジェット燃焼にする、図7流線型理論燃焼室4Q1〜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狙い過熱蒸気噴射ノズル6A噴射で、内部燃焼ガス吸引噴射+ジェット燃焼+前方の空気を吸引噴射して、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88B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88B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 hydrogen injection in the theoretical combustion chamber 4Q, aiming at increased oxygen and hydrogen combustion in the ultra-high pressure extreme combustion of the oxygen combined jet airplane 39T, is driven by the vertical all-blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extreme Liquid oxygen 5K + electricity + high temperature water is received from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D of low-cost electric manufacture, and the theoretical combustion chamber 4Q is shown in FIG. 7 streamlined theoretical combustion chamber 4Q1 in which air 28a around the leading theoretical combustion chamber 4Q is taken as intake air passage 5b and fuel injection combustion is performed from a plurality of fuel injection nozzles 6X to intake air or the like, resulting in rocket combustion + jet combustion. -Select a plurality according to the application, liquid oxygen 5K compression, air volume compression work rate of 21/60000 volume compression work rate, 200MPa superheated steam injection nozzle 6A injection, internal combustion gas suction injection + jet combustion + sucking and injecting forward air, rocket combustion + jet combustion, and propelling by jet combustion, and when going up into the universe, it will be a variety of airplanes that return to space by rocket combustion, Oxygen combined air injection unit 88B Super high pressure mass combustion 100 times output aim, enabling a day trip anywhere on the earth such as 16 rounds of space use in the space use prime day near fuel cost 0, CO2 exhaust at the same speed in the atmosphere 1/10 Fuel Cost 1/10 Operating Profit Margin Various energy storage cycle coalescence engines and coalescence methods are used, aiming for an oxygen coalescence air injection unit 88B, aiming 10 times that of existing airplanes.

図13酸素合体プロペラ飛行機39Uの超高圧極限燃焼で酸素水素増大燃焼狙う、図5理論燃焼室4Q理論膨張機関3Qプロペラ7A駆動は、竪型全動翼比重大物質重力タービン8Q燃料費0発電極端に安価電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備3Dから、液体酸素5K+電気+高温水を受給して、液体圧縮で200MPa狙いとし、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4Q内壁燃料加熱管1L+高温水加熱管5H+酸素加熱管5Fで最適温度に加熱し、最適温度の過熱蒸気50や燃料や酸素にして、過熱蒸気制御弁25+酸素制御弁24D+燃料制御弁25bを開放し、超高圧燃料酸素中心付近複数3000℃以上燃焼にして、過熱蒸気50の一部を燃焼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、内壁の保護燃焼や超高圧高温燃焼にして、200MPa狙い過熱蒸気50を過熱蒸気噴射ノズル6A噴射し、燃焼ガス噴射ノズル6Y燃焼ガス49を吸引噴射して、圧縮吸入空気路5b空気噴射ノズル5の圧縮空気部9D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3Q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度外周方向噴射で理論膨張機関3Q駆動し、横軸1hによりプロペラ7A駆動や回転翼7B駆動にして、大気中同一速度CO2排気1/10燃料費1/10狙いにし、運用利益率も既存飛行機の10倍狙うプロペラ飛行機等にして、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 hydrogen increased combustion with ultra high pressure extreme combustion of oxygen combined propeller plane 39U, Fig. 5 Theoretical combustion chamber 4Q Theoretical expansion engine 3Q propeller 7A drive is a vertical all-blade ratio critical material gravity turbine 8Q fuel cost 0 power generation extreme Receives liquid oxygen 5K + electricity + high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, and aims at 200 MPa by liquid compression, liquid oxygen control valve 5T + liquid fuel control Open the valve 1K + water control valve 5Q, heat it to the optimum temperature with the theoretical combustion chamber 4Q inner wall fuel heating pipe 1L + high temperature water heating pipe 5H + oxygen heating pipe 5F, and use the superheated steam 50, fuel and oxygen at the optimum temperature to overheat Open steam control valve 25 + oxygen control valve 24D + fuel control valve 25b and burn at 3000 ° C. or more near super high pressure fuel oxygen center and part of superheated steam 50 near combustion center With the aim of suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion, protective combustion of the inner wall and ultra-high pressure high temperature combustion, 200MPa target superheated steam 50 is injected with superheated steam injection nozzle 6A, and combustion gas injection nozzle 6Y combustion gas 49 is suctioned and injected. The theoretical expansion engine which sucks and injects the compressed air portion 9D air of the compressed intake air passage 5b and the fuel injection nozzle 6X and greatly increases the fuel injection combustion combustion amount from the fuel injection nozzle 6X, thereby increasing the fuel combustion amount. 3Q driving, combustion gas 49 as high-pressure high-temperature combustion gas 49, theoretical expansion engine 3Q driving by circumferential direction injection of 380 degrees in the circumferential direction from the center, propeller 7A driving or rotor blade 7B driving by the horizontal axis 1h, in the atmosphere Combined with the combined oxygen and Fig. 12 with the same speed CO2 exhaust 1/10 aiming at fuel cost 1/10 and the operating profit rate aiming 10 times as much as the existing airplane. To propeller jet airplane 39N, to a variety of energy storage cycle combined institutions and coalescence method.

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8Q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、ウォータージェット加工機の水噴射速度マッハ3以上に真空中の重力加速度を追加し、仕事率が速度に比例+高さに比例するため、水銀噴射速度マッハ3以上+真空中の重力加速度=マッハ30等極限速度駆動狙いとして、100倍速度1/100質量垂直水銀駆動+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8Q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 gravity-type gravity turbine 8Q power generation of vertical type moving blades, aiming at a resource price of 0 fuel cost of 0 power generation less than 1/2 of nuclear power generation, water jet processing Since the gravity acceleration in the vacuum is added to the water injection speed Mach 3 or more of the machine, and the work rate is proportional to the speed + proportional to the height, the mercury injection speed Mach 3 or more + gravity acceleration in the vacuum = Mach 30 ultimate speed 100x speed 1/100 mass vertical mercury drive + all-blade horizontal axis 1h counter-rotating drive to maximize the power of gravity acceleration of 9.8m / second in the world, to the world's highest building height of 828m There is a possibility of extremely low-priced power generation with a vertical all-blade specific material gravity turbine 8Q power generation with 200 sets of vertical equipment, one power generation, and the same amount of mercury generated 2710 times that of the existing pumped-storage 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8Q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 resources, zero fuel costs, and zero power generation to less than half of nuclear power generation, large-scale blade-like material gravity turbine 8Q power generation is compared with existing thermal power nuclear steam turbine power generation in the process of comparison with 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8Q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 8Q 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8Q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3Qや酸素合体水噴射部88Lや酸素合体空気噴射部88B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 8Q power generation Extremely inexpensive power generation, as an electric product prime, 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 the air volume compression work rate, the theoretical expansion engine 3Q, the oxygen combined water injection unit 88L and the oxygen combined air injection unit 88B 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24〜200MPa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24〜200MPa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(気体の体積は圧力に反比例する理論で最良機関+酸素水素増大燃焼狙う) 3Q:理論膨張機関(ボイルの法則で最良機関+真空中の最高加速駆動狙う) 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24〜200MPa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、 4L:理論膨張機関自動車、 4Q:理論燃焼室(超高圧理論燃焼狙う) 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:高温水加熱管、 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(6種類の円筒タービン動翼群嵌合組立+磁気利用軸受荷重0接近にする) 8N:竪型全動翼比重大物質重力タービン(6種類の円筒タービン動翼群嵌合組立+磁気利用軸受荷重0接近にする) 8R:横型全動翼水重力タービン(円筒タービン翼群直列対向同期回転+磁気利用軸受荷重0接近にする) 8S:横型全動翼比重大物質重力タービン(円筒タービン翼群直列対向同期回転+磁気利用軸受荷重0接近にする) 8P:竪型全動翼水重力タービン(6種類の円筒タービン動翼群嵌合組立+磁気利用軸受荷重0接近+超高速外周速度にする) 8Q:竪型全動翼比重大物質重力タービン(6種類の円筒タービン動翼群嵌合組立+磁気利用軸受荷重0接近+超高速外周速度にする) 8T:横型全動翼水重力タービン(円筒タービン翼群直列対向同期回転+磁気利用軸受荷重0接近+超高速外周速度にする) 8U:横型全動翼比重大物質重力タービン(円筒タービン翼群直列対向同期回転+磁気利用軸受荷重0接近+超高速外周速度にする) 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、 9Q:垂直平行板(噴射空気を保存船尾に誘導する垂直平行の板) 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、 39Q:酸素合体スクリュー船舶、 39R:酸素合体噴射船舶、 39S:酸素合体スクリュー噴射船舶、 39T:酸素合体噴射飛行機、 39U:酸素合体プロペラ飛行機、 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、 51:合流抽出器(合流するための抽出器) 51A:空気抽出室、 52a:高温水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、 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) 88B:酸素合体空気噴射部(超高圧ロケット燃焼+ジェット燃焼+過熱蒸気噴射吸引) 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) 88L:酸素合体水噴射部(超高圧ロケット燃焼+ジェット燃焼+過熱蒸気噴射吸引) 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 24 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, fuel injection combustion, and injected or exhausted) 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 24-200 MPa combustion gas, and fuel injection multistage combustion is driven during expansion to drive a 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 (the gas volume is inversely proportional to the pressure, aiming at the best engine + oxygen-hydrogen-enhanced combustion) 3Q: Theoretical expansion engine (Boile's) 3R: Theoretical gas turbine (theoretical best gas turbine whose gas volume is inversely proportional to the pressure) 3S: Theoretical steam turbine (the gas 3T: Theoretical gas compressor (theoretical best gas compressor whose gas volume is inversely proportional to the pressure) 3U: Theoretical turbine, 3V: Pump engine (existing various pumps in the engine) Use) 3X: Compressor engine (uses various 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, liquid nitrogen and fuel injection) 3a: water-repellent plating, 3b: water-repellent coating, 4F: combustion gas reciprocating engine, 4H: Heat absorption tube (long-lens 2d collects sunlight into a heat absorption tube in a straight line and heats the air temperature inside the tube to the maximum, and the outside air temperature also rises) 4J: Battery drive wheel, 4K: Theoretical expansion engine vehicle, 4L: Theoretical expansion engine vehicle, 4Q: Theoretical combustion chamber (targeted for ultra-high pressure theoretical combustion) 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (high temperature combustion in water vapor to thermally decompose water 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 part, 5: air injection nozzle, 5a: high-pressure high-temperature combustion gas control valve, 5b: compression intake air passage, 5d: combustion flow inner wall, 5e: ultra-high pressure oxygen, 5A: supply air Valve, 5B: Cooling fin, 5C: Exhaust chamber, 5D: Exhaust valve, 5E: Air supply chamber, 5F: Oxygen heating tube, 5G: Steam heating tube, 5H: High temperature 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 control 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 (specific gravity using liquid specific critical substance 3E pressure and specific gravity difference) 6X: Fuel injection nozzle, 6X: After burner (combustion with the intake air flow combined with the fuel injection cold heat 28a combustion flow 6Y, and the space rises due to a large increase in the amount of fuel combustion) 6Y: Burning gas injection nozzle (cooling 28a combustion flow) 6Z: Water vapor injection nozzle, 7A: Propeller, 7B: Rotary blade, 7C: Screw, 8c: Turbine blade (inner and outer rotor blade groups are respectively cylindrical parts of the inner and outer shaft devices) 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 (small large output stage annular same diameter approximately the same shape approximately the same length screw assembly 9 as rotation stopper fixed all rotor blades rotating in opposite directions are supported 8H: Vertical-type all-blade turbine (selection of cemented carbide or turbine blades coated with silicon resin or fluororesin) 8H: Vertical-type full-blade water gravity turbine (existing steam turbine) Is dammed with stationary vanes Because the output approaches 0, all moving blades are essential, and the work rate is 1 / 360,000 of platinum sphere. Compressed heat is recovered with a pump + compression heat recovery unit, and divided storage turbine drive is used for heating and cooling + used in various applications) 8H: Vertical type full-blade hydrogravity turbine (When using thermal drive + cooling drive, the head of use is 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 shaft 1h) 8L: Critical material ratio of the vertical type moving blade 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 all blade water gravity turbine (six kinds of cylindrical turbine blade group fitting assembly + magnetism) Use bearing load close to 0) 8N : Vertical all blade ratio material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load close to 0) 8R: Horizontal all blade hydrogravity turbine (cylindrical turbine blade group series opposed synchronous) 8S: Horizontal type full blade ratio material gravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic type bearing load close to 0) 8P: Vertical type full blade dynamic gravity Turbine (six types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load 0 approach + super high speed peripheral speed) 8Q: vertical type full blade ratio material gravity turbine (six types of cylindrical turbine blade group fitting) 8T: Horizontal full-blade hydrogravity turbine (cylindrical turbine blade group series counter-synchronous rotation + approach to magnetic bearing load 0 approach + ultra-high speed peripheral speed) 8U: Horizontal type Blade specific gravity material gravity turbine (cylindrical turbine blade group serial opposed synchronous rotation + magnetic bearing load approach 0 + super high speed outer peripheral speed) 9: Wear-resistant annular assembly (specific material flow path including 8c is made of cemented carbide only 9A: Cylindrical annular assembly (wear-resistant cylindrical annular assembly blade group with 6 types of moving blade group for simple structure, few parts, fully automated machining, easy assembly, easy weight reduction, etc. 9A: Cylindrical annular assembly (inner 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 annular blade 60H + outlet fixed inner blade 60K is fitted. 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9Q: Vertical parallel plate (injecting the blast air to the storage stern) Hanging 10: Hull, 10A: Ship cabin, 10b: Control room, 10c: Control room, 10d: Guest room, 10e: Cargo compartment, 11D: Gas cooling room, 16B: Vertical axis, 21: Solar heater (An intake air passage is also provided in the heat absorption pipe 4H for main use) 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 (superheated steam 50 with compressed air calorie by compressing air 28a with a heat pump) 28b: Compressed air calorie, 28A: Intake air path, 28B: Air path inlet, 38: Rotating guide, 38a: Flight trunk, 38b: Compressed air 28a containing hot oxygen + liquid oxygen and liquid nitrogen Wing, 38c: flying wing, 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 plane, 39B: Solar thermal gravity rotating plane, 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 39L: oxygen coalescence propeller airplane, 39N: oxygen coalescence propeller airplane, 39P: oxygen coalescence rotorcraft, 39Q: oxygen coalescence screw ship, 39R: oxygen coalescence injection ship, 39S: oxygen Combined screw injection ship, 39T: Combined injection airplane, 39U: Oxygen combined propeller airplane, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheated steam chamber, 50: Heat (compressed air 28a with a heat pump and heated by compressed air 50A: water vapor, 50a: superheated steam injection pipe, 51: air extractor, 51: confluence extractor (extractor for confluence) 51A: air extraction chamber, 52a: High temperature water 52a: Deep ocean water, 52b: High temperature water, 52d: Heat (change from 50) 52e: Cold heat (change from 28a) 55B: Transmission, 60A: Inner shaft device (equipment with turbine blades) 60B: Outer shaft device (Turbine blade equipped device) 60C: Cylindrical inner moving blade group (Wear resistant cylindrical annular assembly fixed moving blade group including fully automatic processing easy assembly) 60D: Cylindrical outer moving Blade group (Wear resistant cylindrical annular assembly fixed rotor blade group including fully automatic machining easy assembly) 60E: Entrance fixed outer blade (inlet blade for annular assembly fixing outer rotor group) 60F: Entrance fixed inner blade ( 60G: Outer annular blade (intermediate blade for annular assembly of outer rotor blade group) 60H: Inner annular blade (intermediate blade for annular assembly of inner rotor blade group) 60J: Outlet fixing Outer blade (exit blade for annular assembly fixing outer rotor blade group) 60K: Outlet fixed inner blade (exit blade for annular assembly fixing inner rotor blade group) 76: gear device (including magnetic friction power transmission device) 77B: half Cylindrical outer box, 77F: injection section outer casing, 77G: cylindrical rotating section, 77a: turbine outer casing, 80: bearing (including magnetic bearing + air bearing) 80a: thrust bearing (including magnetic bearing + air bearing) 80A: joint 80B: Fastener, 80Y: Liquid air suction Pulling water jet (high pressure high temperature combustion gas 5M receiving high pressure high temperature steam chamber 5N, fuel injection combustion in 5M multiple times, 5N heated and injected multiple times from the inner circumference and inner circumference outer circumference, air suction jet and water 80Z: 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, 5N is heated multiple times from the inner circumference and inner circumference outer circumference several times Injecting, fuel injection combustion injection to a plurality of locations of air suction flow, air suction injection and water suction injection) 84: Counter-rotating magnetic friction device (fixed portion inner blade group and outer blade group) 84Y: Counter-rotating gear device (device that counter-rotates with existing technology) 85: Counter-rotating magnetic device (magnet-use gear height from slight to non-contact with 1h gear on the horizontal axis) Mutual reverse rotation) 8 Y: Counter-rotating gear device (reciprocally reverse rotation with the existing horizontal shaft 1h gear) 88A: Oxygen combined air injection unit (rocket injection + jet combustion + steam injection and combined injection) 88B: Oxygen combined air injection unit (super High pressure rocket combustion + jet combustion + superheated steam injection suction) 88K: Oxygen combined water injection part (rocket combustion + jet combustion + steam injection and combined injection) 88L: Oxygen combined water injection part (super high pressure rocket combustion + jet combustion + superheat) 95a: Combustion gas reservoir, 95b: Compressed air reservoir, 95c: Superheated steam reservoir, 103: Cold heat recovery device,

Claims (377)

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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 gravity turbines (8Q). 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 21 to 40 sets of various energy 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)とした磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 41-60 sets of various energy 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)とした磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 61-80 sets of various energy 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)とした磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 81 to 100 sets of energy 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)とした磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 101-120 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 121 to 140 sets of various energy storage cycle coalescing 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 141 to 160 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 types of blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 161-180 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 blades each with wear-resistant super-water-repellent plating (3a), a cylindrical ring assembly (9A), a magnetic bearing load of 0 approach + super-high-speed circumferential speed specific material Gravity turbine (8Q) 181 to 200 sets of various energy 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) 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 (8Q) with high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) Various energy storage cycle coalescence engines and coalescence methods for generating power from 21 to 40 sets of vertical turbine moving blade ratio critical material gravity turbine (8Q) at a high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) 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 (8Q) with high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) 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 (8Q) 61-80 with a high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) 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 (8Q) 81-100 set at a high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) Various energy storage cycle coalescing engine and coalescence method for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8Q) 101-120 set at a high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) Various energy storage cycle coalescence engine and coalescence method for generating a power generation of a vertical type all-blade ratio critical material gravity turbine (8Q) 121-140 set at a high circumferential speed. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) Various energy storage cycle coalescence engine and coalescence method for generating a power generation with a high-speed circumferential speed and a vertical all blade ratio critical material gravity turbine (8Q) 141-160 set. 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1〜30で噴射駆動する磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 wear bearing load 0 approach + super high, each of which is a wear-resistant super water-repellent plating (3a), and which is driven by a specific material (3E) Mach 1-30 with six types of moving blade groups having a cylindrical annular assembly (9A) Various energy storage cycle coalescing engine and coalescence method for generating a power generation of a vertical all-blade ratio critical material gravity turbine (8Q) 161-180 set at a high circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30, injection inlet fixed outer wing (60E) + outer Annular blade (60G) + Outlet fixed outer blade (60J) fitted to the outside of the cylinder and moving to the outside of the cylinder. Magnetic bearing load approaching 0 + Super high speed peripheral speed ratio material gravity turbine (8Q) 181 ~ Various energy storage cycle coalescence engines and coalescence methods 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 1 to 20 sets of saddle-type all-blade ratio critical material gravity turbine (8Q) with driving magnetic bearing load approaching 0 + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 power to 21-40 sets of saddle type all-blade ratio critical material gravity turbine (8Q) with driving magnetic bearing load approaching 0 + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 41 to 60 sets of saddle type full blade ratio gravity material gravity turbine (8Q) with driving magnetic bearing load approaching 0 + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 saddle-type all-blade ratio critical material gravity turbine (8Q) with driving magnetic bearing load approaching 0 + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 vertical type moving blade ratio critical material gravity turbine (8Q) 81 to 100 with a magnetic bearing load to be driven approaching 0 and an ultra-high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 power generation by using a vertical type moving blade ratio critical material gravity turbine (8Q) 101-120 sets with a driving magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 ratio critical material gravity turbine (8Q) 121-140 sets with a magnetic bearing load to be driven approaching 0 and an ultra-high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 full-blade ratio critical material gravity turbine (8Q) 141-160 with a magnetic bearing load to be driven approaching 0 and an ultra-high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 full-blade ratio critical material gravity turbine (8Q) 161-180 set to drive magnetic bearing load 0 approach + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds 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 ratio critical material gravity turbine (8Q) 181 to 200 sets having a magnetic bearing load of 0 approaching + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 engines and coalescence methods for generating 21 to 40 sets of saddle-type full blade ratio critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engines and coalescence methods for generating power from 61 to 80 sets of vertical turbine blade critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engines and coalescence methods for generating power of 81 to 100 sets of saddle-type full blade ratio critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engine and coalescence method for generating power of 101 to 120 sets of vertical turbine moving blade ratio critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 power of 121-140 sets of saddle-type full blade ratio critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engine and coalescence method for generating power to a power generator with a total gravity of a vertical turbine blade (8Q) 141 to 160 set at 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engine and coalescence method for generating a power generation of a vertical type moving blade ratio critical material gravity turbine (8Q) 161-180 set to 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 coalescence engine and coalescence method for generating power to a power generator of a vertical type moving blade ratio critical material gravity turbine (8Q) 181 to 200 set to 0 approach + super high speed circumferential speed. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load approaching 0 + super high speed peripheral speed specific material gravity turbine (8Q) 1-20 sets of various energy conservation cycle coalescence engine to generate power And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven magnetic bearing load approaching 0 + super high speed circumferential speed of the blade-type all blade ratio critical material gravity turbine (8Q) 21-40 sets of various energy conservation cycle coalescence engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by using magnetic bearing load 0 approach + super high speed peripheral blade ratio critical material gravity turbine (8Q) 41-60 sets of various energy conservation cycle combined engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed peripheral speed specific material gravity turbine (8Q) 61-80 sets of various energy conservation cycle combined engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed circumferential speed with a large blade ratio critical material gravity turbine (8Q) 81-100 sets of various energy conservation cycle coalescence engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed circumferential speed of a blade-type all blade ratio critical material gravity turbine (8Q) 101-120 sets of various energy conservation cycle coalescence engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed peripheral speed specific material gravity turbine (8Q) 121-140 combination various energy conservation cycle coalescence engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by magnetic use bearing load 0 approach + super-high speed peripheral speed blade-type critical material gravity turbine (8Q) 141-160 sets of various energy conservation cycle combined engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Reversing drive and generator (1) driven magnetic bearing load approaching zero + super high speed peripheral speed ratio material mass turbine (8Q) 161-180 sets of various energy conservation cycle coalescence engine And coalescing 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 30 with 6 types of moving blade groups (9A) made of wear-resistant super-water-repellent plating (3a), respectively. Inverted drive and generator (1) Driven by using magnetic bearing load of 0 approach + super high speed peripheral speed specific material gravity turbine (8Q) 181-200 sets of various energy conservation cycle combined engine And coalescing 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed peripheral speed blade type critical material gravity turbine (8Q) 1-20 sets of various energy conservation cycle coalescence engine and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Driven by magnetic bearing load to drive 0 type + super-high speed circumferential speed of all blade ratio critical material gravity turbine (8Q) 21-40 sets of various energy storage cycle coalescence engine and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed circumferential speed, all-blade ratio critical material gravity turbine (8Q) 41-60 sets of various energy storage cycle coalescence engine and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Magnetically utilized bearing load to drive 0 type + full-speed blade ratio critical material gravity turbine (8Q) with a super high speed circumferential speed (8Q) 61-80 sets of various energy conservation cycle coalescence engines and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and power generator (1) Driven by magnetic bearings to be driven near zero load + super high speed circumferential speed with a large blade ratio critical material gravity turbine (8Q) 81-100 sets of various energy storage cycle coalescence engines and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and power generator (1) Driven by magnetic bearings to be driven near zero load + super-high speed circumferential speed of a large blade ratio critical material gravity turbine (8Q) 101-120 sets of various energy storage cycle coalescence engines and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and power generator (1) Driven by magnetic bearings to be driven near zero load + super-high speed circumferential speed, full-scale blade ratio critical material gravity turbine (8Q) 121-140 sets of various energy storage cycle coalescing engines and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and power generator (1) Driven by magnetic use bearing load 0 approach + super high speed circumferential speed of the blade type critical blade gravity material gravity turbine (8Q) 141-160 sets of various energy storage cycle coalescence engine and Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Magnetically utilized bearing load to drive (1) Type of full-scale blade ratio critical material gravity turbine (8Q) 161-180 sets with super high speed circumferential speed Merge 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30狙い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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Double reversal on the horizontal axis (1h) driven by Mach 30 aiming at specific material (3E) with 6 kinds of moving blade groups (9A) and wear-resistant super water-repellent plating (3a), respectively. Drive and generator (1) Driven by magnetic use bearing load 0 approach + super high speed circumferential speed with a large blade ratio critical material gravity turbine (8Q) 181-200 sets of various energy storage cycle coalescence engine and Merge 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive 1 to 20 sets of vertical mass moving blade ratio critical material gravity turbine (8Q) with a magnetic reversal bearing load of 0 approaching + super high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 21-40 sets with a magnetic utilization bearing load 0 approaching + super high speed circumferential speed driven by counter-rotating drive and generator (1) on the horizontal axis (1h) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive 41 to 60 sets of vertical full-blade ratio critical material gravity turbines (8Q) with a magnetic bearing load approaching 0 and ultra-high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 61-80 sets with a magnetic reversal bearing load 0 approach + super high speed circumferential speed driven by counter-rotating drive or generator (1) on the horizontal axis (1h) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 81 to 100 sets with a magnetic reversal bearing load 0 approach + super high speed circumferential speed driven by counter rotating drive or generator (1) on the horizontal axis (1h) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 101-120 pairs with a magnetically applied bearing load 0 approaching + super high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 121-140 sets with magnetically applied bearing load 0 approaching + super high speed circumferential speed driven by counter rotation on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 141-160 sets with a magnetic utilization bearing load 0 approaching + super high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 161-180 sets with a magnetic reversal bearing load 0 approaching + super high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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30狙いで噴射比重大物質(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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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-phase blade assembly (9A) made of wear-resistant super-water-repellent plating (3a), specific-critical material (3E) Mach 30 aiming injection ratio critical material (2E) mixed injection acceleration drive Vertically rotating blade ratio critical material gravity turbine (8Q) 181 to 200 sets with a magnetic reversal bearing load 0 approach + super high speed circumferential speed driven by counter-rotating drive or generator (1) on the horizontal axis (1h) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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), cylindrical material assembly (9A), specific material (3E) Mach 1-30, injection ratio critical material (2E) mixed injection acceleration drive 1 to 20 sets of vertical mass moving blade ratio critical material gravity turbine (8Q) with a magnetic reversal bearing load of 0 approaching + super high speed circumferential speed driven by counter rotating on the horizontal axis (1h) and generator (1) Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 21-40 with double reversal drive on the horizontal axis (1h) to be driven and magnetic bearing load to drive the generator (1) approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 41-60 with double reversal drive on the horizontal axis (1h) to drive and magnetically utilized bearing load to drive the generator (1) + close to super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically moving blade ratio critical material gravity turbine (8Q) 61-80 with double reversal drive on the horizontal axis (1h) to drive and magnetism bearing load to drive generator (1) approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 81-100 with double reversal drive on the horizontal axis (1h) to be driven and magnetic utilization bearing load to drive the generator (1) 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 101-120 with double reversal drive on the horizontal axis (1h) to be driven and magnetism bearing load to drive the generator (1) 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 121-140 with a double reversal drive on the horizontal axis (1h) to be driven and a magnetic utilization bearing load to drive the generator (1) 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 141-160 with a double reversal drive on the horizontal axis (1h) to drive and a magnetically utilized bearing load to drive the generator (1) 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 161-180 with a double reversal drive on the horizontal axis (1h) to drive and a magnetically utilized bearing load to drive the generator (1) 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined 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1〜30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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 1-30 with 6 kinds of moving blade groups made into cylindrical annular assembly (9A), each made of wear-resistant super water-repellent plating (3a) Vertically rotating blade ratio critical material gravity turbine (8Q) 181 to 200 with a horizontal reversal drive (1h) of double reversal drive and generator (1) drive using magnetic bearing load 0 approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method for combined power generation. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 turbine (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 turbine (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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). Two or more energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of gravity turbine (8Q) significant material gravity turbine (8Q) with a magnetic bearing load of 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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. Two or more energy storage cycle coalescence engines and coalescence methods for generating 1 to 200 sets of gravity turbine (8Q) significant material gravity turbine (8Q) with a magnetic bearing load of 0 approach + super high speed circumferential speed. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 turbine (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 turbine (8Q) having a magnetic bearing load of 0 approaching + super high speed circumferential speed 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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) Reversing direction of rotation to minimize resonance and noise. Magnetically utilized bearing load approaching 0 + super high speed peripheral speed ratio material mass turbine (8Q) 1 to 200 sets Various energy storage cycle coalescence engines and coalescence methods for generating electricity. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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) A vertical all-blade blade with a rotation of the rotating direction opposite to that of the inner shaft device (60A) and a counter-rotating rotation of the rotating blade group (60D). Various energy conservation cycle coalescence engine and coalescence method for generating 1 to 200 sets of specific material gravity turbine (8Q). 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 vertical-type full-blade ratio critical material gravity turbine (8Q) equipped with a solar heater (21) with buoyancy on the water surface, and using solar heated air with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed 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 coalescing engine and coalescence method for high temperature water to 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、太陽光加熱空気を磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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. Vertically moving blade ratio critical material gravity turbine (8Q) with 0 approach + super high speed circumferential speed (8Q) Compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, for each compression Various energy storage cycle coalescence engines and coalescence methods that recover heat from a 1 to multi-stage compression heat recovery device (2C) to make electricity + liquid air cold heat + hot water to superheated steam temperature 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、太陽光加熱空気を磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 has a vertical all-blade ratio critical material with solar heated air approaching a magnetic bearing load of 0 and an ultra-high speed circumferential speed. Gravity turbine (8Q) Extremely inexpensive electricity-driven electric drive, 1 to multi-stage heat pump (1G) compresses suction multiple times, 1 to multi-stage compression heat recovery unit (2C) recovers heat for each compression, + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment (3D) Various energy storage cycle coalescence engine and coalescence method. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 (8Q) with maximum air (28a) temperature, magnetic bearing load approaching 0 + super high speed circumferential speed 1 to multi-stage heat pump of extremely low cost electric power generation electric drive Various (1G) suction multiple times compression, heat recovery with 1 to multi-stage compression heat recovery device (2C) for each compression, to make electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) Energy conservation cycle coalescence engine and coalescence Method. 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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). The air (28a) temperature is maximized, and the external air (28a) is also heated. Each air passage (28A) is selected as a high temperature selective suction, and the magnetic bearing load is approached + super high speed circumferential speed ratio is significant. Mass gravity turbine (8Q) Extremely inexpensive power generation electric drive, 1 to multi-stage heat pump (1G) compressed by suction multiple times, and for each compression heat recovery by 1 to multi-stage compression heat recovery device (2C), Electricity + liquid air cooling + hot water to overheating Various energy conservation cycle combined institutions and coalescence how to temperature heat supply facilities (3D). 太陽光加熱器(21)を平地に円形鉄道を設けて具備して、太陽光加熱空気を磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 vertical all-blade ratio critical material gravity turbine (8Q) with a solar heater (21) provided with a circular railroad on a flat ground, and solar heated air with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. ) Extremely inexpensive electricity-driven electric drive, 1 to multi-stage heat pump (1G) compresses several times with suction, 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 engine and coalescence method to make high temperature water to 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、太陽光加熱空気を磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 (8Q) with a load approaching 0 and an ultra-high speed circumferential speed (8Q) Compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, 1 to various energy storage cycle coalescence engines and coalescence methods that recover heat with a multi-stage compression heat recovery device (2C) to make electricity + liquid air cold heat + hot water to 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 device that controls the rotation of sunlight at a right angle in the vertical direction is used. Mass gravity turbine (8Q) Extremely inexpensive power generation electric drive, 1 to multi-stage heat pump (1G) compressed by suction multiple times, and for each compression heat recovery by 1 to multi-stage compression heat recovery device (2C), Various energy storage cycle coalescence engine and coalescence method to make electricity + liquid air cold heat + hot water to 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、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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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). Vertically moving blade ratio critical material gravity turbine (8Q) with maximum irradiation internal air (28a) temperature, magnetic utilization bearing load approaching 0 + super high speed circumferential speed 1 to multiple stages of extremely inexpensive power generation electric drive Compressed several times with a heat pump (1G) and recovered heat with 1 to multi-stage compression heat recovery unit (2C) for each compression, to electricity + liquid air cold heat + hot water to superheated steam temperature supply equipment (3D) Various energy storage cycle coalescing machines And coalescence 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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+高温水〜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 all-blade with maximum temperature of the internal air (28a) irradiated and the external air (28a) heated to each air passage (28A) as a high-temperature selective suction with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed Specific gravity material gravity turbine (8Q) Extremely inexpensive power generation electric drive, 1 to multi-stage heat pump (1G) compresses suction multiple times, and each compression recovers heat with 1 to multi-stage compression heat recovery unit (2C) Electricity + liquid air cold + high temperature Various energy saving cycles combined engine and coalescence process for the ~ superheated steam heat supply facilities (3D). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D), various energy storage cycle coalescence engines and coalescence methods for collecting superheated steam hot-injected methane into methane hydrate on the seabed. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D), various energy storage cycle coalescence engines and coalescence methods for recovering superheated steam hot-injected methane with liquid nitrogen (5L) cooled liquid methane to methane hydrate on the sea floor. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D), various energy conservation cycle coalescence engines and coalescence methods for recovering superheated steam hot-injected methane into methane hydrate under permafrost. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D), various energy storage cycle coalescence engines and coalescence methods for recovering superheated steam hot-injected methane into methane hydrate under permafrost with liquid nitrogen (5L) cooled liquid methane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D), various energy conservation cycle coalescence engines and coalescence methods that provide superheated steam heat injection enclosures in methane hydrate under permafrost to make methane recovery and pasture grazing projects. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that are received from 3D) and recovered by providing a superheated steam injection enclosure in the oil sand zone. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that are received from 3D) and recovered by providing a superheated steam injection enclosure in the oil shale zone. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy conservation cycle coalescence engines and coalescence methods that are received from 3D) and recovered by providing a superheated steam injection enclosure in an old oil extraction zone. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that are received from 3D) to receive low-priced superheated steam in the food manufacturing industry, etc., and make mass production of inexpensive food products. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper superheated steam and use it for agricultural, industrial, industrial, or mining industries to make the best use of thermal energy. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Various energy storage cycle coalescence engines that drive the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and drive the vehicle, and Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) Various energy storage cycles that drive the automobile by driving the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at ultra high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression. 1) Various energy storage cycle coalescence engines and coalescence methods that store electricity in the drive storage battery (1A) and drive the storage battery drive wheels (4J) rotation theoretical expansion engine automobile (4L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity and storing in the theoretical expansion engine (3Q) driven generator (1) driven storage battery (1A) as the theoretical combustion chamber (4Q) ultra high pressure fuel combustion aiming at ultra high pressure combustion Then, various energy storage cycle coalescence engines and coalescence methods for driving storage battery drive wheels (4J) rotation theory expansion engine automobile (4L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) Drive generator (1) Drive storage battery (1A ) And storage battery drive wheel (4J) rotation theoretical expansion engine automobile (4L) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at ultra high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression. 1) Various energy storage cycle coalescence engines and coalescence methods for storing in the drive storage battery (1A) and driving the theoretical expansion engine automobile (4L) capable of rotating the storage battery drive wheels (4J) and normal wheels. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity and storing in the theoretical expansion engine (3Q) driven generator (1) driven storage battery (1A) as the theoretical combustion chamber (4Q) ultra high pressure fuel combustion aiming at ultra high pressure combustion Then, various energy storage cycle coalescence engines and coalescence methods for driving the theoretical expansion engine automobile (4L) capable of rotating the battery drive wheels (4J) and rotating the normal wheels. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) Drive generator (1) Drive storage battery (1A ) And various energy storage cycle coalescence engines and coalescence methods for driving a theoretical expansion engine automobile (4L) capable of rotating a storage battery drive wheel (4J) and rotating a normal wheel. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動して理論膨張機関自動車(4L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims to receive ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engine and coalescence method for driving an expansion engine vehicle (4L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion Combusting the theoretical expansion engine (3Q) as super high pressure fuel combustion and screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving a rotating ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity, drives the theoretical expansion engine (3Q) as ultrahigh pressure fuel combustion, and various energy to drive the screw (7C) rotating ship Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) aiming for ultra high pressure combustion, theoretical expansion engine (3Q) as ultra high pressure fuel combustion, screw (7C) rotating ship drive Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Then, various energy storage cycle coalescence engines and coalescence methods for driving a screw (7C) multiple rotation ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple-rotation ship as ultra-high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as super high pressure fuel combustion and screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving a screw (7C) multi-rotation oxygen coalescence screw ship (39Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen as ultra-high pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving coalescence screw ship (39Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as super high pressure fuel combustion and screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation oxygen coalescence screw ship (39Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動して酸素合体スクリュー船舶(39Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) to make the compression volume 21/60000 of the air compression. Theoretical combustion chamber (4Q) aimed at ultra high pressure combustion. The oxygen is driven by the theoretical expansion engine (3Q) as ultra high pressure fuel combustion. Various energy storage cycle coalescence engine and coalescence method for driving coalescence screw ship (39Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動してスクリュー(7C)回転酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion Combusting the theoretical expansion engine (3Q) as super high pressure fuel combustion and screw (7C) Rotating oxygen coalescence water injection unit (88L) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動してスクリュー(7C)回転酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and screw (7C) rotary oxygen combined water injection unit (88L) 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動してスクリュー(7C)回転酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) aiming for ultra-high pressure combustion, driving theoretical expansion engine (3Q) as ultra-high pressure fuel combustion, screw (7C) rotating oxygen coalescence Various energy storage cycle coalescing engine and coalescence method for driving water injection part (88L) jet propulsion ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving a screw (7C) multi-rotation oxygen coalescence water injection part (88L) injection propulsion ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen as ultra-high pressure fuel combustion Combined water injection unit (88L) injection propulsion ship, various energy storage cycle combining engine and combining method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as super high pressure fuel combustion and screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation oxygen coalescence water injection part (88L) injection propulsion ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)噴射推進酸素合体スクリュー噴射船舶(39S)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving a screw (7C) multi-rotation oxygen coalescence water injection section (88L) injection propulsion oxygen coalescence screw injection vessel (39S). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)噴射推進酸素合体スクリュー噴射船舶(39S)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen as ultra-high pressure fuel combustion Combined water injection unit (88L) injection propulsion oxygen combination screw injection ship (39S) various energy storage cycle combination engine and combination method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(88L)噴射推進酸素合体スクリュー噴射船舶(39S)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as super high pressure fuel combustion and screw (7C) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation oxygen coalescence water injection section (88L) injection propulsion oxygen coalescence screw injection ship (39S). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動して酸素合体水噴射部(88L)噴射推進酸素合体スクリュー噴射船舶(39S)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) to make the compression volume 21/60000 of the air compression. Theoretical combustion chamber (4Q) aimed at ultra high pressure combustion. The oxygen is driven by the theoretical expansion engine (3Q) as ultra high pressure fuel combustion. Combined water injection unit (88L) injection propulsion oxygen combination screw injection ship (39S) various energy storage cycle combination engine and combination method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber aiming at streamlined ultra-high pressure combustion receiving low-priced liquid oxygen (5K) and making the compression volume 21/60000 of air compression (4Q) Oxygen combined water injection unit with multiple ultra-high pressure fuel combustion injection propulsion (88L) 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) + electricity and aims at streamlined ultra-high pressure combustion (4Q) oxygen combined water injection part (88L) injection propulsion ship driven by a variety of ultra-high pressure fuel combustion injection propulsion Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進とした酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) + electricity + hot water and aims at streamlined ultra-high pressure combustion (4Q) oxygen combined water injection part (88L) injection propulsion ship Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) receiving a cheaper liquid oxygen (5K) and making the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving the oxygen coalescence water injection part (88L) injection propulsion ship. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined water injection part (88L) which receives cheap liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction flow path with a streamlined ultra-high pressure combustion as a multiple ultra-high pressure fuel combustion injection propulsion 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at streamlined ultra-high pressure combustion (4Q) Oxygen combined water injection unit with air suction flow path and multiple ultra-high pressure fuel combustion injection propulsion (88L) 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)噴射推進酸素合体噴射船舶(39R)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) receiving a cheaper liquid oxygen (5K) and making the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving the oxygen coalescence water injection part (88L) injection propulsion oxygen coalescence injection ship (39R). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)噴射推進酸素合体噴射船舶(39R)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined water injection part (88L) which receives cheap liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction flow path with a streamlined ultra-high pressure combustion as a multiple ultra-high pressure fuel combustion injection propulsion Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion oxygen coalescence injection ship (39R). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88L)噴射推進酸素合体噴射船舶(39R)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at streamlined ultra-high pressure combustion (4Q) Oxygen combined water injection unit with air suction flow path and multiple ultra-high pressure fuel combustion injection propulsion (88L) Various energy storage cycle coalescence engines and coalescence methods for driving a jet propulsion oxygen coalescence injection ship (39R). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)複数とした酸素合体水噴射部(88L)噴射推進酸素合体噴射船舶(39R)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper liquid oxygen (5K) and sets the compression volume to 21/60000 of air compression. Streamlined ultra-high pressure combustion aiming at the theoretical combustion chamber (4Q) multiple oxygen combined water injection part (88L) injection propulsion oxygen Various energy storage cycle coalescence engine and coalescence method for driving the coalescence injection ship (39R). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber aiming at streamlined ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Oxygen combined air injection unit with multiple ultra-high pressure fuel combustion injection propulsion (88B) Various energy storage cycle coalescence engines and coalescence methods for making an injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) aiming for streamlined ultra-high pressure combustion, oxygen combined air injection part (88B) injection propulsion aircraft made into multiple ultra-high pressure fuel combustion injection propulsion Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at streamlined ultrahigh pressure combustion (4Q) oxygen combined air injection unit (88B) injection propulsion airplane Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) receiving a cheaper liquid oxygen (5K) and making the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for making an oxygen coalescence air injection unit (88B) injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection unit (88B) that receives low-priced liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction channel that aims at streamlined ultra-high pressure combustion and includes multiple ultrahigh-pressure fuel combustion injection propulsion 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection unit that receives low-priced liquid oxygen (5K) + electricity + high-temperature water and has a superficial combustion chamber (4Q) air suction flow path that aims at streamlined ultra-high pressure combustion and has multiple ultra-high pressure fuel combustion injection propulsion (88B) Various energy storage cycle coalescence engines and coalescence methods for making an injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)噴射推進酸素合体噴射飛行機(39T)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) receiving a cheaper liquid oxygen (5K) and making the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving the oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence injection airplane (39T). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)噴射推進酸素合体噴射飛行機(39T)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection unit (88B) that receives low-priced liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction channel that aims at streamlined ultra-high pressure combustion and includes multiple ultrahigh-pressure fuel combustion injection propulsion Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence aircraft (39T). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、流線型超高圧燃焼狙う理論燃焼室(4Q)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(88B)噴射推進酸素合体噴射飛行機(39T)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection unit that receives low-priced liquid oxygen (5K) + electricity + high-temperature water and has a superficial combustion chamber (4Q) air suction flow path that aims at streamlined ultra-high pressure combustion and has multiple ultra-high pressure fuel combustion injection propulsion (88B) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence aircraft (39T). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする流線型超高圧燃焼狙う理論燃焼室(4Q)複数とした酸素合体空気噴射部(88B)噴射推進酸素合体噴射飛行機(39T)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-cost liquid oxygen (5K) is received and the compression volume is 21/60000 of air compression. Streamlined ultra-high pressure combustion aiming at the theoretical combustion chamber (4Q) multiple oxygen combined air injection unit (88B) injection propulsion oxygen Various energy storage cycle coalescence engine and coalescence method for driving a coalescence jet airplane (39T). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and propeller (7A) Various energy storage cycle coalescence engines and coalescence methods for driving a rotating airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) The energy that drives the theoretical expansion engine (3Q) as the ultra-high pressure fuel combustion and drives the propeller (7A) rotating airplane Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming at ultra high pressure combustion, driving theoretical expansion engine (3Q) as ultra high pressure fuel combustion, propeller (7A) rotating airplane drive Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Then, a propeller (7A) various energy storage cycle coalescing engine and coalescence method for driving a multi-turn airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive as propulsion (7A) multiple rotation airplane Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39U)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. And various energy storage cycle coalescence engines and coalescence methods for driving a propeller (7A) multi-rotation oxygen coalescence propeller airplane (39U). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39U)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and propeller (7A) multiple rotation oxygen as ultra-high pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a coalescence propeller airplane (39U). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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(39U)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives as propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a multi-rotation oxygen coalescence propeller airplane (39U). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動してプロペラ(7A)回転酸素合体プロペラ飛行機(39U)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and propeller (7A) Various energy storage cycle coalescence engines and coalescence methods for driving a rotary oxygen coalescence propeller airplane (39U). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at ultra high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. 7B) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive by airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) aiming for ultra-high pressure combustion, theoretical expansion engine (3Q) driving rotor blades (7B) rotating as a high-pressure fuel combustion Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretically rotating engine (3Q) driven rotor blade (7B) rotates as an ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescing engine and coalescence method for rotating the rotor (7B) and driving the airplane by multiple rotations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion, the theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) multiple rotations as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving an airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) + electricity + high-temperature water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive the aircraft. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for rotating the rotor blade (7B) and driving the oxygen coalescence rotor blade airplane (39P). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion, the theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) multiple rotations as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods for driving oxygen coalescence rotorcraft (39P). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) + electricity + high-temperature water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive oxygen coalesced rotorcraft (39P). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at ultra high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. 7B) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive an oxygen coalescence rotorcraft (39P). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動プロペラ(7A)回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at super high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression The propeller (7A) ) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive the oxygen coalescence air injection part (88B) injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動プロペラ(7A)回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) aimed at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) drive propeller (7A) rotates as an ultrahigh pressure fuel combustion and oxygen combined air injection part ( 88B) Various energy storage cycle coalescing engines and coalescence methods for driving jet propulsion airplanes. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動プロペラ(7A)回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) aiming for ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) drive propeller (7A) rotates as oxygen combined air Various energy storage cycle coalescence engine and coalescence method for driving an injection unit (88B) jet propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescing engines and coalescence methods for driving a propeller (7A) a plurality of times and driving an oxygen coalescence air injection part (88B) injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive propellers (7A) multiple rotations to combine oxygen Various energy storage cycle coalescing engine and coalescence method for driving air injection unit (88B) jet propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive propeller (7A) multiple revolutions Oxygen coalescence air injection unit (88B) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion airplane. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving the propeller (7A) multiple times and driving the oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence propeller injection airplane (39N). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive propellers (7A) multiple rotations to combine oxygen Various energy storage cycle coalescence engine and coalescence method for driving air injection part (88B) injection propulsion oxygen coalescence propeller jet airplane (39N). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)1〜複数駆動プロペラ(7A)複数回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive propeller (7A) multiple revolutions Various energy storage cycle coalescence engines and coalescence methods for driving the oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence propeller injection airplane (39N). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)超高圧燃料燃焼として理論膨張機関(3Q)駆動プロペラ(7A)回転し酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) driven by ultra high pressure combustion aiming at super high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression The propeller (7A) ) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive the oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence propeller injection airplane (39N). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(5M)を噴射して理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method in which a high pressure high temperature combustion gas (5M) is injected from a combustion gas injection nozzle (6Y) to drive a theoretical expansion engine (3Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(5M)を噴射して理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure high-temperature combustion gas control valve (5a) Higher pressure than the open combustion gas injection nozzle (6Y) Various energy storage cycle coalescence engines and coalescence methods for injecting high-temperature combustion gas (5M) to drive a theoretical expansion engine (3Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(5M)を噴射して理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y ) Various energy storage cycle coalescence engines and coalescence methods that drive a theoretical expansion engine (3Q) by injecting higher pressure and high temperature combustion gas (5M). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion High-pressure and high-temperature combustion gas (5M) is injected from the combustion gas injection nozzle (6Y) to drive the theoretical expansion engine (3Q) in which the upper expansion blade (8d) and the lower expansion blade (8e) are reversed in the horizontal axis (1h). Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure high-temperature combustion gas control valve (5a) Higher pressure than the open combustion gas injection nozzle (6Y) Various energy storage cycle coalescence engine and coalescence method for driving a theoretical expansion engine (3Q) in which high temperature combustion gas (5M) is injected and 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y ) Various energy storage cycle coalescence engines that drive a high-pressure high-temperature combustion gas (5M) and drive the upper expansion blade (8d) and the lower expansion blade (8e) in the horizontal axis (1h) and doubly reverse (3Q) And coalescing method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion High pressure high temperature combustion gas (5M) is injected from the combustion gas injection nozzle (6Y), and the upper expansion blade (8d) and the lower expansion blade (8e) are turned into the horizontal axis (1h) and the counter rotating assembly turbine blade (8f) is assembled. Various energy storage cycle coalescence engine and coalescence method for driving expansion engine (3Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure high-temperature combustion gas control valve (5a) Higher pressure than the open combustion gas injection nozzle (6Y) Various energies for injecting high-temperature combustion gas (5M) to drive the upper expansion blade (8d) and the lower expansion blade (8e) on the horizontal axis (1h), the counter-rotating assembly turbine blade (8f), and the theoretical expansion engine (3Q) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) open combustion gas injection nozzle (6Y ) High-pressure high-temperature combustion gas (5M) is injected to drive the upper expansion blade (8d) and lower expansion blade (8e) to the horizontal axis (1h), the counter-rotating assembly turbine blade (8f), and the theoretical expansion engine (3Q) drive. Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(5M)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion The air suction combustion amount is increased, the high-pressure high-temperature combustion gas (5M) is injected from the combustion 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 coalescing engine and coalescence method for driving a theoretical expansion engine (3Q) for assembly of blades (8f). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods for a theoretical expansion engine (3Q) that expands and expands in the circumferential direction by 380 degrees. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) The high-pressure high-temperature combustion gas control valve (5a) The theory of expanding and expanding 380 degrees in the circumferential direction Various energy storage cycle coalescence engine and coalescence method for expansion engine (3Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high-pressure combustion (4Q) High-pressure and high-temperature combustion gas control valve (5a) open 380 degrees in the circumferential direction Various energy storage cycle coalescing engines and coalescence methods for expanding the theoretical expansion engine (3Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves a maximum drive speed by expanding 380 degrees in the circumferential direction. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure and high-temperature combustion gas control valve (5a) Open maximum in the circumferential direction by 380 degrees expansion Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3Q) for driving speed. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high-pressure combustion (4Q) High-pressure and high-temperature combustion gas control valve (5a) open 380 degrees in the circumferential direction Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3Q) that achieves maximum drive speed by expansion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves a maximum driving speed by expansion at 380 degrees in the circumferential direction and double inversion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves maximum driving speed with multiple reversals. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high-pressure combustion (4Q) High-pressure and high-temperature combustion gas control valve (5a) open 380 degrees in the circumferential direction Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves maximum drive speed by expansion and counter rotation. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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にする超高圧燃焼狙う理論燃焼室(4Q)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(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) opened as ultra high pressure fuel combustion Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that is double-reversed with expansion of 380 degrees in the circumferential direction. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Ultra-high pressure that receives cheap liquid oxygen (5K), compresses liquid together with liquid fuel (1c) and water (52a), and injects and burns ultra-high-pressure compressed fuel with air compression of 21/60000 volume, etc. Various energy storage cycle coalescing engine and coalescence method for a theoretical combustion chamber (4Q) aimed at combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper liquid oxygen (5K) + electricity, compresses liquid together with liquid fuel (1c) and water (52a), and burns with ultra-high pressure compressed fuel injection with a compression volume of 21/60000 volume of air compression, etc. Various energy storage cycle coalescence engine and coalescence method for a theoretical combustion chamber (4Q) aimed at ultra high pressure combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, compressing liquid together with liquid fuel (1c) and water (52a), and compression volume is ultra-high pressure compressed fuel with air compression of 21/60000 volume, etc. Various energy storage cycle coalescing engine and coalescence method for a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion for injection combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), liquid compression with liquid fuel (1c) and water (52a), and various energy storage cycles that heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming for ultra high pressure combustion Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, compressing liquid together with liquid fuel (1c) and water (52a), and heating to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming at ultra high pressure combustion Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper liquid oxygen (5K) + electricity + hot water, compresses it with liquid fuel (1c) and water (52a), and heats it to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming for ultra-high pressure combustion Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper liquid oxygen (5K), compresses liquid together with liquid fuel (1c) and water (52a), and heats oxygen control valve (24D) to the optimum temperature at the inner wall of the theoretical combustion chamber (4Q) aiming for ultra high pressure combustion ) + Fuel control valve (25b) + superheated steam control valve (25) to open various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Cheap oxygen oxygen (5K) + electricity is received and compressed with the liquid fuel (1c) and water (52a) to compress the liquid and aim at ultra-high pressure combustion Heating the oxygen control valve to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) (24D) + Fuel control valve (25b) + superheated steam control valve (25) to open various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper liquid oxygen (5K) + electricity + hot water, compresses it with liquid fuel (1c) and water (52a), and heats it to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming for ultra-high pressure combustion Various energy storage cycle coalescence engines and coalescence methods for opening the oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、液体燃料(1c)や水(52a)と共に液体圧縮して超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + hot water, compressing liquid together with liquid fuel (1c) and water (52a), and controlling oxygen heating to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming for ultra high pressure combustion Various energy storage cycle coalescence engines and coalescence methods for injecting the valve (24D) + fuel control valve (25b) + superheated steam control valve (25) together with the open received superheated steam. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)を加熱する超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receive cheaper liquid oxygen (5K), 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 engine and coalescence method to make the theoretical combustion chamber (4Q) aiming at ultra high pressure combustion that heats the outer superheated steam (50) by combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)を加熱する超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, 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 engine and coalescence method to make the theoretical combustion chamber (4Q) aiming at ultra high pressure combustion that heats the outer superheated steam (50) by combustion at ℃ or higher. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、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)を加熱する超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, open oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature Various energy storage cycle coalescence engine and coalescence method to make the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that heats the outer superheated steam (50) by combustion in the vicinity of 3000 ° C. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receive cheaper liquid oxygen (5K), 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 for heating the outer superheated steam (50) by combustion to a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion aiming at the suction pyrolysis electrolysis near the center. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, 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 that heat the outer superheated steam (50) by combustion at ℃ or higher and make a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion aiming at the suction pyrolysis electrolysis near the center. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, open oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature Various energy storage cycle coalescing engines and coalescence methods that make superheated combustion (4Q) aiming at super high pressure combustion aiming at heating part of the peripheral superheated steam (50) by combustion near 3000 ° C in the vicinity and heating partly near the center. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receive cheaper liquid oxygen (5K), 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 for heating the superheated steam (50) at the periphery by combustion to a theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at combustion by suction pyrolysis electrolysis oxygen hydrogen increase combustion near the center. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity, 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 that heat the outer superheated steam (50) by combustion at ℃ or higher and make the theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at increased combustion by suction pyrolysis electrolysis oxygen hydrogen hydrogen near the center. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + hot water, open oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature Heating peripheral superheated steam (50) in the vicinity of more than 3000 ° C combustion, and various energy storage cycle coalescence engines to make a theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at suction pyrolysis electrolysis oxygen hydrogen increase combustion near the center, and Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、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超高圧燃焼狙う理論燃焼室(4Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receive cheaper liquid oxygen (5K) + hot water, and open the oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Combining various energy storage cycles into a theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at increased thermal absorption of pyrolysis, electrolysis, oxygen, hydrogen and hydrogen near the center of heating with peripheral superheated steam (50) including superheated steam received by combustion at 3000 ° C or higher Organization and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and using a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion as a streamlined type, a combustion gas (49) injection accelerating injection oxygen combined water injection part (88L) provided in series Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-priced liquid oxygen (5K) + electricity is received, and the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined and has a plurality of series combustion gas (49) oxygen-accelerated water injection unit (88L) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, the combustion chamber (49) injection accelerating injection oxygen injection water injection unit equipped with multiple theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion and streamlined (88L) various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) with a plurality of series combustion chambers (4Q) with a streamlined theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion (4Q) and oxygen on the inner wall of combustion flow (5d) + Energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) that uses fuel + superheated steam heated at an optimum temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Combustion gas (49) equipped with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity and aim at ultra-high pressure combustion as a streamline type (4Q) inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that uses oxygen + fuel + superheated steam of an optimal temperature heated. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received less expensive liquid oxygen (5K) + electricity + hot water, and the combustion chamber (4Q) and the combustion flow inner wall (4Q) with combustion gas (49) equipped with multiple theoretical combustion chambers (4Q) aimed at ultra-high pressure combustion and streamlined (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) that uses oxygen + fuel + superheated steam heated at an optimal temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) with a plurality of series combustion chambers (4Q) with a streamlined theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion (4Q) and oxygen on the inner wall of combustion flow (5d) + Energy storage cycle coalescence engine and coalescence method with oxygen coalescence water injection part (88L) for the combustion of theoretical combustion chamber (4Q) aiming at super high pressure combustion by heating the fuel + superheated steam at the optimum temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Combustion gas (49) equipped with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity and aim at ultra-high pressure combustion as a streamline type (4Q) inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) for the ideal combustion chamber (4Q) combustion, etc., which is heated at an optimal temperature by heating the oxygen + fuel + superheated steam of the gas to the theoretical combustion chamber (4Q). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received less expensive liquid oxygen (5K) + electricity + hot water, and the combustion chamber (4Q) and the combustion flow inner wall (4Q) with combustion gas (49) equipped with multiple theoretical combustion chambers (4Q) aimed at ultra-high pressure combustion and streamlined (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) for the theoretical combustion chamber (4Q) combustion, etc., in which the oxygen + fuel + superheated steam of (5d) is heated to an optimum temperature and aimed at ultrahigh pressure combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)内壁や燃焼流内壁(5d)の酸素+燃料+受給高温水を含む過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + high-temperature water, the combustion chamber (4Q) and combustion flow inner wall (5d ) Oxygen + Fuel + Receiving high-temperature water superheated steam is heated to an optimal temperature to make it a theoretical combustion chamber (4Q) combustion aiming at ultra high pressure combustion, etc. Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion at 3000 ° C or higher. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) aimed at superheated steam suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) aimed at combustion with superheated steam suction pyrolysis electrolysis oxygen hydrogen augmentation in multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis oxygen oxygen hydrogen combustion with multiple combustion at 3000 ° C or higher. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) for heating and injecting superheated steam (50) of the combustion flow inner wall (5d) high-temperature water heating pipe (5H). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion at 3000 ° C or more. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + high temperature water is received and oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C Various energy storage cycle coalescence engines and coalescence with the oxygen coalescence water injection section (88L) for heating and injecting the superheated steam (50) including the superheated steam received from the combustion flow inner wall (5d) and the high-temperature water heating pipe (5H) Method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined water injection unit that receives low-priced liquid oxygen (5K) and injects combustion into the air (28a) at the optimum suction suction flow location in the same manner as the theoretical combustion chamber (4Q) aiming at a plurality of streamline type ultrahigh pressure combustion (4Q) 88L), various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined water injection that receives cheaper liquid oxygen (5K) + electricity, and also injects the air (28a) into the optimum location of the suction injection flow with a plurality of streamlined ultrahigh pressure combustion aiming combustion chambers (4Q) Part (88L) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen that receives cheaper liquid oxygen (5K) + electricity + high-temperature water, and has a theoretical combustion chamber (4Q) that aims at a plurality of streamlined ultrahigh pressure combustions in the air (28a) suction injection optimum location as well. Various energy storage cycle coalescence engine and coalescence method in the coalescence water injection part (88L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods which receive cheaper liquid oxygen (5K) and expand the air inlet to the oxygen coalescence water injection section (88L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity and expand the air inlet forward by using an oxygen coalescence water injection unit (88L). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity + high temperature water and have an oxygen coalescence water injection section (88L) that expands the air inlet forward. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), using the oxygen coalescence water injection part (88L), expanding the air inlet forward, approaching a straight line, and maximally injecting bubbles into the ship bottom, various energy storage cycle coalescence engines and coalescence methods . 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines that receive cheaper liquid oxygen (5K) + electricity, expand the air inlet toward the straight line by making the oxygen coalescence water injection part (88L) close to a straight line, and inject the bubbles to the bottom of the ship at the maximum, and Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy conservation cycles that receive cheaper liquid oxygen (5K) + electricity + hot water, oxygen combined water injection part (88L), expand the air inlet forward, approach the straight line, and inject maximum bubbles to the bottom of the ship Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、酸素合体水噴射部(88L)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy conservation cycle coalescence engines that receive cheaper liquid oxygen (5K) + high-temperature water, make the oxygen coalesced water injection part (88L) expand the air inlet forward, approach the straight line, and inject maximum bubbles into the ship's bottom And coalescing method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined, and a plurality of in-line combustion gas (49) injection acceleration injection oxygen combined air injection section (88B) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Cheaper liquid oxygen (5K) + electricity is received, and the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined and has a plurality of series combustion gas (49) oxygen combined air injection unit (88B) for accelerated injection Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined, and a plurality of series combustion gas (49) oxygen combined air injection unit for accelerated injection (88B) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) with a plurality of series combustion chambers (4Q) with a streamlined theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion (4Q) and oxygen on the inner wall of combustion flow (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) that uses + fuel + superheated steam heated to an optimum temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Combustion gas (49) equipped with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity and aim at ultra-high pressure combustion as a streamline type (4Q) inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalesced air injection section (88B) that uses oxygen + fuel + superheated steam heated at an optimal temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received less expensive liquid oxygen (5K) + electricity + hot water, and the combustion chamber (4Q) and the combustion flow inner wall (4Q) with combustion gas (49) equipped with multiple theoretical combustion chambers (4Q) aimed at ultra-high pressure combustion and streamlined (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) that uses oxygen + fuel + superheated steam heated at an optimum temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) with a plurality of series combustion chambers (4Q) with a streamlined theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion (4Q) and oxygen on the inner wall of combustion flow (5d) + Energy storage cycle coalescence engine and coalescence method in the oxygen coalescence air injection part (88B) for the combustion of the theoretical combustion chamber (4Q) aiming at super high pressure combustion by heating the fuel + superheated steam at the optimum temperature. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Combustion gas (49) equipped with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity and aim at ultra-high pressure combustion as a streamline type (4Q) inner wall and combustion flow inner wall (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) for theoretical combustion chamber (4Q) combustion, etc., in which the oxygen + fuel + superheated steam is heated at an optimum temperature to aim at ultrahigh pressure combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)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超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received less expensive liquid oxygen (5K) + electricity + hot water, and the combustion chamber (4Q) and the combustion flow inner wall (4Q) with combustion gas (49) equipped with multiple theoretical combustion chambers (4Q) aimed at ultra-high pressure combustion and streamlined (5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) for the theoretical combustion chamber (4Q) combustion, etc., in which oxygen + fuel + superheated steam of (5d) is heated at an optimum temperature and aimed at ultrahigh pressure combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、超高圧燃焼狙う理論燃焼室(4Q)を流線型として複数直列具備の燃焼ガス(49)で(4Q)内壁や燃焼流内壁(5d)の酸素+燃料+受給高温水を含む過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)燃焼等にする酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + high-temperature water, the combustion chamber (4Q) and combustion flow inner wall (5d ) Oxygen + Fuel + Superheated steam containing received high-temperature water is heated to an optimal temperature to make it a theoretical combustion chamber (4Q) combustion aiming at ultra-high pressure combustion, etc. Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence air injection part (88B) aimed at superheated steam suction pyrolysis electrolysis. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion at 3000 ° C or higher. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection part (88B) aimed at superheated steam suction pyrolysis electrolysis oxygen oxygen hydrogen augmentation combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at combustion with superheated steam suction pyrolysis electrolysis oxygen hydrogen augmentation in multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at combustion with superheated steam suction pyrolysis electrolysis oxygen hydrogen hydrogen increase combustion at a temperature of 3000 ° C or more. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K), the oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more combustion Various energy storage cycle coalescence engines and coalescence methods in which an oxygen coalescence air injection section (88B) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall to aim at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) for heating and injecting superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)の過熱蒸気(50)を加熱噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the superficial combustion chamber (4Q) near the center oxygen fuel combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) that heat-inject superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion at 3000 ° C or more. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、夫々の内壁で酸素+燃料+過熱蒸気を最適温度加熱して超高圧燃焼狙う理論燃焼室(4Q)中心付近酸素燃料燃焼3000℃以上複数燃焼で燃焼流内壁(5d)高温水加熱管(5H)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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretical liquid oxygen (5K) + high temperature water is received and oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall to aim at super high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C Various energy storage cycle coalescence engines and coalescence with an oxygen coalescence air injection section (88B) that heats and injects superheated steam (50) including superheated steam received in the combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion. Method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection unit that receives cheaper liquid oxygen (5K), and also injects air (28a) into the optimum location of the suction injection flow, and also has a plurality of streamlined ultrahigh pressure combustion aiming combustion chambers (4Q). 88B), various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen combined air injection that receives cheaper liquid oxygen (5K) + electricity, and also injects the air (28a) into the optimum location of the suction injection flow with a plurality of streamlined ultrahigh pressure combustion aiming combustion chambers (4Q) (88B) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、空気(28a)吸引噴射流最適箇所にも複数の流線型超高圧燃焼狙う理論燃焼室(4Q)具備同様に燃焼噴射する酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Oxygen that receives cheaper liquid oxygen (5K) + electricity + high-temperature water, and has a theoretical combustion chamber (4Q) that aims at a plurality of streamlined ultrahigh pressure combustions in the air (28a) suction injection optimum location as well. Various energy storage cycle coalescence engine and coalescence method in the coalescence air injection section (88B). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) and rotating the oxygen coalescence air injection section (88B) to enable vertical ascent and descent, and various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity and rotate the oxygen coalescence air injection section (88B) to enable vertical ascent and descent. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, and rotating various oxygen storage air injection sections (88B) to enable vertical ascending and descending, and various energy storage cycle combining engines and combining methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) and rotate the oxygen coalescence air injection section (88B) to enable reverse injection. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity and rotate the oxygen coalescence air injection section (88B) to enable reverse injection. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水を受給して、酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity + hot water and rotate the oxygen coalescence air injection section (88B) to enable reverse injection. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水を受給して、酸素合体空気噴射部(88B)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + hot water and rotate the oxygen coalescence air injection section (88B) to enable reverse injection. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various types of electric-driven theoretical gas compressors (3T) that receive cheaper electricity + hot water (52b) and compress the gas volume from the outer peripheral long compressor blade to the central short compressor blade with the gas volume inversely proportional to the pressure. Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines that receive less expensive electricity and are electrically driven theoretical gas compressors (3T) that compress the gas volume from the outer peripheral long large compression blades to the central short compression blades with the gas volume inversely proportional to the pressure, and Merge method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low energy electricity + superheated steam, and various energy storage cycles as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blade to the central short compression blade with the gas volume inversely proportional to the pressure Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + hot water (52b), and compresses air 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 for suction compression. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving cheaper electricity, various energy storage that sucks and compresses air as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blades to the central short compression blades, whose gas volume is inversely proportional to pressure Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + superheated steam, and sucks and compresses 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 in inverse proportion to the pressure Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + hot water (52b), and compresses air 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 for producing suction compression heat exchange superheated steam. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Theoretically compressed heat exchange superheated steam that takes in air as an electrically driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades in inverse proportion 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-cost electricity + superheated steam is received, and the volume of the gas is compressed proportionally to the pressure, and the compressed air is compressed as heat from an air-driven theoretical gas compressor (3T) that compresses from the outer peripheral large compression blade to the central short compression blade. Various energy storage cycle coalescence engine and coalescence method for producing exchange superheated steam. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Electrically driven theoretical gas compressor (3T) that receives cheaper electricity + hot water (52b) + superheated steam and compresses the volume of gas from the outer peripheral large compression blade to the central short compression blade with the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam by sucking air as 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + hot water (52b), and compresses air 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 coalescing engine and coalescence method for producing superheated steam in a suction compressed air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives compressed air from an air-driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which are inversely proportional to the pressure. Various energy storage cycle coalescence engine and coalescence method for producing superheated steam in a vessel (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-cost electricity + superheated steam is received, and air is sucked and compressed as an electrically driven theoretical gas compressor (3T) that compresses gas 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 producing superheated steam with an air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + hot water (52b), and compresses air 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 for supplying superheated steam to the production and supply facility (3D) with a suction compressed air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives compressed air from an air-driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which are inversely proportional to the pressure. Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production and supply equipment (3D) in the vessel (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-cost electricity + superheated steam is received, and air is sucked and compressed as an electrically driven theoretical gas compressor (3T) that compresses gas 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 engines and coalescence methods for supplying superheated steam to the production supply facility (3D) with an air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives cheaper electricity + hot water (52b), and compresses air 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 for supplying compressed air + superheated steam to the production supply facility (3D) with a suction compressed air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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。   Vertically moving blade ratio critical material gravity turbine (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives compressed air from an air-driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which are 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low-cost electricity + superheated steam is received, and air is sucked and compressed as an electrically driven theoretical gas compressor (3T) that compresses gas 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 engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) with an air heat exchanger (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Electrically driven theoretical gas compressor (3T) that receives cheaper electricity + hot water (52b) + superheated steam and compresses the volume of gas from the outer peripheral large compression blade to the central short compression blade with the gas volume inversely proportional to the pressure Various energy storage cycle coalescing engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) with a suction compressed air compressor (2Y). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure In compliance, various energy storage cycle coalescing engines and coalescing methods configured to compress from the outer peripheral large compression blade (8) to the central short compression blade (8). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) as a observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) as a configuration for compression from the outer peripheral long large compression blade (8) to the central short compression blade (8) as a observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) from the outer circumference to the suction center as a configuration in which the outer circumference long large compression blade (8) is compressed to the central short compression blade (8) as a observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed water from the outer circumference to the suction center as a configuration for compressing the outer circumference long large compression blade (8) to the center short compression blade (8) as a observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods in which air (28a) compressed high-temperature water is heated from the outer circumference to the suction center as a configuration in which compression is performed from the outer peripheral long large compression blade (8) to the central short compression blade (8) as observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume 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 as a configuration for compressing from the outer circumferential long large compression blade (8) to the central short compression blade (8) as observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure As a structure to compress from the outer peripheral long large compression blade (8) to the center short compression blade (8), the air (28a) is compressed from the outer periphery to the suction center, and various energy storage cycle coalesced heats are compressed and compressed air heat exchanger (2Y). Organization and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycles in which high-temperature water is heated by the compressed air heat exchanger (2Y) from the outer periphery to the suction center as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) as a observance. Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Various energy storage cycles in which the superheated steam is heated from the outer periphery to the suction center by the air (28a) compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume 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 compressing the outer peripheral long large compression blade (8) to the central short compression blade (8) as observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure 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 the outer peripheral long large compressor blade (8) to the central short compressor blade (8) as observance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure 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 compressing from the outer peripheral long large compression blade (8) to the central short compression blade (8) as a compliance. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure In compliance, various energy storage cycle coalescence engines and coalescence that produce ultra-high pressure compressed air + ultra-high pressure superheated steam with compressed air heat exchanger (2Y) as a configuration that compresses from the outer peripheral large compression blade (8) to the central short compression blade (8) Method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure Combined with various energy storage cycle to supply compressed air + superheated steam production and supply equipment (3D) with compressed air heat exchanger (2Y) as a configuration to compress from the outer peripheral large compression blade (8) to the central short compression blade (8) Organization and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure In compliance, the energy is supplied to the high pressure compressed air + high pressure superheated steam production and supply facility (3D) using the compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8). Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure As a configuration, the compressed air heat exchanger (2Y) supplies the ultra high pressure compressed air + ultra high pressure superheated steam production and supply equipment (3D) as a configuration that compresses from the outer peripheral large compression blade (8) to the central short compression blade (8). Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure As a compliance, various types of energy storage are provided to supply liquid air + super-high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration that compresses from the outer peripheral large compression blade (8) to the central short compression blade (8). Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure As a configuration, the compressed air heat exchanger (2Y) supplies the liquid oxygen + liquid nitrogen + ultra-high pressure superheated steam production / supply facility (3D) as a configuration for compressing the outer peripheral large compression blade (8) to the central short compression blade (8). Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) Theoretical gas compressor (3T) of extremely inexpensive power generation electric drive, gas volume is inversely proportional to pressure In compliance, the compressed air heat exchanger (2Y) is configured to compress electricity + liquid oxygen + liquid nitrogen + ultra-high pressure superheated steam production and supply equipment (3D) as a configuration that compresses from the outer peripheral large compression blade (8) to the central short compression blade (8). Various energy storage cycle coalescence engines and coalescence methods to be supplied. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving less expensive liquid oxygen (5K) fuel injection combustion, various energy storage cycles in which fuel pipe (25a) extended upper expansion blade group (8d) fuel injection combustion from multiple locations in the circumferential 380 degree expansion process Merger engine and merger method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving less expensive liquid oxygen (5K) + electricity, fuel injection combustion, various energy that fuel injection combustion from multiple locations of fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential direction 380 degrees expansion process Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Fuel injection combustion with cheaper liquid oxygen (5K) + electricity + high-temperature water received, and fuel injection combustion from multiple locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receiving less expensive liquid oxygen (5K) and injecting and burning, and in the process of expansion in the circumferential direction of 380 degrees, the fuel injection (25a) extended upper expansion blade groups (8d) increase the amount of fuel injection combustion combustion from a plurality of locations Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Fuel injection combustion that receives cheaper liquid oxygen (5K) + electricity, and increases the fuel injection combustion combustion amount from multiple locations of the fuel pipe (25a) extended upper expansion blade group (8d) in the expansion process in the circumferential direction of 380 degrees Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Fuel injection combustion with cheaper liquid oxygen (5K) + electricity + high-temperature water received, and fuel injection combustion from multiple locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees Various energy storage cycle coalescence engines and coalescence methods that increase the amount of combustion. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescence methods that receive and inject and burn cheaper liquid oxygen (5K) and compress air 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+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engine and coalescence method for receiving cheaper liquid oxygen (5K) + electricity and fuel injection combustion, and compressing air between the outer casing (77a) in the circumferential direction of 380 degrees expansion . 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Low energy liquid oxygen (5K) + electricity + high temperature water received fuel injection combustion, various energy storage cycle coalescence engine that compresses air between the outer casing (77a) in the circumferential direction 380 degrees expansion process And coalescing method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Various energy storage cycle coalescence engines and coalescences that receive cheaper liquid oxygen (5K) + high-temperature water and inject and burn fuel and compress the air with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees Method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives and injects cheaper liquid oxygen (5K), and compresses the compressed air portion (9D) with the turbine outer casing (77a) in the circumferential direction of 380 degrees of expansion to compress the air injection nozzle ( 5) Various energy conservation cycle coalescence engines and coalescence methods for injecting at multiple locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Cheaper liquid oxygen (5K) + electricity is received and injected and burned, and compressed air part (9D) is compressed with the turbine outer box (77a) in the circumferential direction of 380 degrees expansion and injected Nozzle (5) Various energy storage cycle coalescence engine and coalescence method for injecting a plurality of locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received fuel injection combustion of cheaper liquid oxygen (5K) + electricity + hot water, and compressed air (9D) with the turbine outer box (77a) in the circumferential expansion process of 380 degrees Air injection nozzle (5) Various energy storage cycle coalescence engine and coalescence method for injecting at a plurality of locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)複数個所噴射燃料燃焼量増大する理論膨張機関(3Q)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives and injects cheaper liquid oxygen (5K), and compresses the compressed air portion (9D) with the turbine outer casing (77a) in the circumferential direction of 380 degrees of expansion to compress the air injection nozzle ( 5) Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that increases the amount of fuel burned at multiple locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Cheaper liquid oxygen (5K) + electricity is received and injected and burned, and compressed air part (9D) is compressed with the turbine outer box (77a) in the circumferential direction of 380 degrees expansion and injected Nozzle (5) Various energy storage cycle coalescence engine and coalescence method for increasing the amount of fuel burned at multiple locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Received fuel injection combustion of cheaper liquid oxygen (5K) + electricity + hot water, and compressed air (9D) with the turbine outer box (77a) in the circumferential expansion process of 380 degrees Air injection nozzle (5) Various energy storage cycle coalescence engine and coalescence method for increasing the amount of fuel combustion at multiple locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Receives and injects cheaper liquid oxygen (5K), and injects and burns fuel from a plurality of locations of the upper upper expansion blade groups (8d) in the fuel pipe (25a) in the expansion process of 380 degrees in the circumferential direction. (77a) Various energy storage cycle coalescing engines and coalescence methods that compress the compressed air portion (9D) and air injection nozzles (5) to increase the fuel combustion quantity at multiple locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Fuel oil is injected and burned with cheaper liquid oxygen (5K) + electricity, 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, and the turbine Various energy storage cycle coalescence engines and coalescence methods in which the compressed air portion (9D) is compressed between the outer box (77a) and the air injection nozzle (5) increases the fuel combustion amount at a plurality of locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+電気+高温水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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) Fuel injection combustion with cheaper liquid oxygen (5K) + electricity + high-temperature water received, and fuel injection combustion from multiple locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees And an energy storage cycle coalescence engine and a coalescence method in which the compressed air portion (9D) is compressed with the turbine outer box (77a) to increase the amount of fuel combustion at the air injection nozzle (5). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)+高温水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)との間で圧縮空気部(9D)空気圧縮して空気噴射ノズル(5)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 (8Q) with magnetic approaching bearing load 0 approach + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply facility (8Q) 3D) receiving cheaper liquid oxygen (5K) + high-temperature water and injecting and burning, and in the process of expansion in the circumferential direction of 380 degrees, fuel injection and combustion is performed from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d), Various energy storage cycle coalescence engines and coalescence methods in which the compressed air portion (9D) is compressed between the turbine outer box (77a) and the air injection nozzle (5) increases the fuel combustion amount at a plurality of locations. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) with a magnetic bearing load of 0 approach + super-high-speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for generating power as a turbine utilizing magnetic force that reversely reverses the group (60C) and the outer cylindrical blade group (60D). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a turbine utilizing magnetic force that double-inverts the blade group (60C) and the cylindrical outer blade group (60D). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a large number of turbines using magnetic force that double-reverses the blade group (60C) and the cylindrical outer blade group (60D). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) with a magnetic bearing load of 0 approach + super-high-speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for generating power as a magnetic force turbine in which the group (60C) and the cylindrical outer rotor blade group (60D) are doubly reversed by the doubly reversed magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a magnetic force turbine in which the rotor blade group (60C) and the cylindrical outer rotor blade group (60D) are doubly reversed by the doubly reversed magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a large number of turbines using magnetic force that double-reverses the rotor blade group (60C) and the cylindrical outer rotor blade group (60D) by the counter-rotating magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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 (8Q) with a magnetic bearing load of 0 approach + super-high-speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for generating power as a weight-supporting magnetic force turbine in which the group (60C) and the cylindrical outer blade group (60D) are doubly reversed by the contra-rotating magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a weight-supporting magnetic force turbine in which the rotor blade group (60C) and the cylindrical outer rotor blade group (60D) are doubly reversed by the contra-rotating magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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。   Magnet type bearing load approaching 0 + super high speed circumferential speed blade-type all blade ratio critical material gravity turbine (8Q) Ultra-high pressure vertical under vacuum mixed material injection including mixed injection and acceleration of gravitational acceleration, inside multiple cylinders Various energy storage cycle coalescence engines and coalescence methods for generating power as a large number of turbines using weight-supported magnetic force such that the rotor blade group (60C) and the cylindrical outer rotor blade group (60D) are doubly reversed by a doubly reversed magnetic device (85). 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetically utilized bearing load approaching 0 + super high speed circumferential speed with vertical blade ratio critical material gravity turbine (8Q) power generation electric product + rocket combustion + jet combustion various energy to drive oxygen combined water injection part (88L) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetized bearing load approaching 0 + super high speed circumferential speed of blade type critical material gravity turbine (8Q) power generation electric product + rocket combustion 2 places + jet combustion 2 places oxygen combined water injection part (88L) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetically-enhanced bearing load approaching 0 + super high speed circumferential speed of a blade-type all-blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 3 locations + jet combustion 3 locations oxygen combined water injection part (88L) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetically-enhanced bearing load 0 approach + super-high speed circumferential speed of vertical blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 4 locations + jet combustion 4 locations oxygen combined water injection part (88L) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetically-enhanced bearing load 0 approach + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 5 locations + jet combustion 5 locations oxygen combined water injection part (88L) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88L)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。   Magnetically utilized bearing load approaching 0 + super-high speed circumferential speed of vertical blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 6 locations + jet combustion 6 locations oxygen combined water injection part (88L) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnetically utilized bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion + various energy to drive oxygen combined air injection unit (88B) as jet combustion Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnet type bearing load approaching zero + super high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 2 locations + jet combustion 2 locations oxygen combined air injection part (88B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnetically-enhanced air injection unit (88B) as a vertical type moving blade ratio critical material gravity turbine (8Q) power generation electrical product + 3 rocket combustion + 3 jet combustion locations Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnetically utilized bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 4 locations + jet combustion 4 locations oxygen combined air injection part (88B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnet type bearing load approaching zero + super high speed circumferential speed with a large blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 5 locations + jet combustion 5 locations oxygen combined air injection part (88B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+超高速円周速度とした竪型全動翼比重大物質重力タービン(8Q)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(88B)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。   Magnetically utilized bearing load approaching zero + super-high speed circumferential speed with full blade ratio critical material gravity turbine (8Q) power generation electrical product + rocket combustion 6 locations + jet combustion 6 locations oxygen combined air injection part (88B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体噴射船舶(39R)にして船底垂直平行板(9Q)内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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy storage cycle coalescing engines and coalescence methods in which a water jet part (88L) driven oxygen coalesced injecting vessel (39R) injects bubbles into the bottom vertical parallel plate (9Q). 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体スクリュー噴射船舶(39S)にして船底垂直平行板(9Q)内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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy storage cycle coalescing engines and coalescence methods in which a water jet part (88L) driven oxygen coalescence screw injection vessel (39S) is used to inject the maximum amount of bubbles into the bottom vertical parallel plate (9Q). 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体噴射船舶(39R)にして船底垂直平行板(9Q)幅広具備して空気浮上量最大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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy storage cycle coalescence engines and coalescence methods that make the water injection part (88L) driven oxygen coalescence injection ship (39R) wide and have a bottom vertical parallel plate (9Q) wide to maximize the amount of air floating. 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体スクリュー噴射船舶(39S)にして船底垂直平行板(9Q)幅広具備して空気浮上量最大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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy storage cycle coalescence engines and coalescence methods that make the water injection part (88L) driven oxygen coalescence screw injection ship (39S) wide and have a bottom vertical parallel plate (9Q) wide to maximize the amount of air floating. 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体噴射船舶(39R)にして船底垂直平行板(9Q)幅広具備して摩擦低減量最大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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy conservation cycle coalescence engines and coalescence methods that maximize the friction reduction amount by making the water injection part (88L) driven oxygen coalescence injection ship (39R) wide in the bottom vertical plate (9Q). 竪型全動翼比重大物質重力タービン(8Q)極端に安価発電電気製造の、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)より安価液体酸素(5K)を受給、酸素合体水噴射部(88L)駆動酸素合体スクリュー噴射船舶(39S)にして船底垂直平行板(9Q)幅広具備して摩擦低減量最大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。   Vertical type moving blade ratio critical material gravity turbine (8Q) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), which is extremely inexpensive power generation electric production, oxygen coalescence Various energy storage cycle coalescence engines and coalescence methods that make the water injection part (88L) driven oxygen coalescence screw injection vessel (39S) wide and provide a bottom vertical parallel plate (9Q) wide to maximize friction reduction.
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